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99942 Apophis

99942 Apophis (provisional designation 2004 MN4) is a near-Earth asteroid and a potentially hazardous object with a diameter of 370 metres (1,210 feet)[3] that caused a brief period of concern in December 2004 when initial observations indicated a probability up to 2.7% that it would hit Earth on April 13, 2029. Additional observations provided improved predictions that eliminated the possibility of an impact on Earth in 2029. Until 2006, a small possibility nevertheless remained that, during its 2029 close encounter with Earth, Apophis would pass through a gravitational keyhole of no more than about 800 kilometres (500 mi) in diameter,[11][12] which would have set up a future impact exactly seven years later on April 13, 2036. This possibility kept it at Level 1 on the Torino impact hazard scale until August 2006, when the probability that Apophis would pass through the keyhole was determined to be very small and Apophis's rating on the Torino scale was lowered to zero. By 2008, the keyhole had been determined to be less than 1 km wide.[11] During the short time when it had been of greatest concern, Apophis set the record for highest rating ever on the Torino scale, reaching level 4 on December 27, 2004.[13]

99942 Apophis
Model of 99942 Apophis's shape, assuming the entire surface is of a similar composition.
Discovery[1]
Discovered by
Discovery siteKitt Peak[1]
Discovery dateJune 19, 2004
Designations
(99942) Apophis
Pronunciation/əˈpɒfəs/, (trad.) /ˈæpəfəs/
Named after
Ἄποφις Apophis
2004 MN4
AdjectivesApophidian /æpəˈfɪdiən/ (Latin Apŏpidis)
Orbital characteristics[1]
Epoch 13 September 2023
(JD 2453300.5)
Uncertainty parameter 0
Observation arc6267 days (17.16 yr)
Earliest precovery dateMarch 15, 2004
Aphelion1.0994 AU (164.47 million km)
Perihelion0.7461 AU (111.61 million km)
0.9227 AU (138.03 million km)
Eccentricity0.19144
0.89 yr (323.7 d)
30.73 km/s
142.9°
1.11198°/day
Inclination3.339°
203.96°
126.60°
Earth MOID0.00026 AU (39 thousand km)
Jupiter MOID4.12 AU (616 million km)
TJupiter6.464
Physical characteristics
Dimensions
  • 0.370 km (0.230 mi)
  • 0.45 × 0.17 km[2]
Mean radius
  • 0.185 km (0.115 mi)
  • 0.17±0.02 km[2]
Mass6.1×1010 kg (assumed)[3]
Mean density
  • ~3.2 g/cm3[4]
  • 2.6 g/cm3 (assumed)[3]
30.4 h (1.27 d)[1][5]
30.55±0.12 h[6]
30.67±0.06 h[7]
Tumbling:[8]
27.38±0.07 h (precession period),[8] 263±6 h (rotation period),[8] 30.56±0.01 h (period of harmonic with strongest lightcurve amplitude)[8]
Temperature270 K
Sq[5]

Preliminary observations by Goldstone radar in January 2013 effectively ruled out the possibility of an Earth impact by Apophis in 2036.[14] By May 6, 2013 (April 15, 2013, observation arc), the possibility of an impact on April 13, 2036 had been eliminated altogether.[3] In 2036, Apophis will approach the Earth at a third the distance of the Sun in both March and December,[1] but this is about the distance of the planet Venus when it overtakes Earth every 1.6 years. On April 12, 2068, the nominal trajectory has Apophis 1.87 AU (280 million km) from Earth.[15] Entering March 2021, six asteroids each had a more notable cumulative Palermo Technical Impact Hazard Scale rating than Apophis, and none of those has a Torino level above 0.[16][a] On average, an asteroid the size of Apophis (370 metres) is expected to impact Earth once in about 80,000 years.[17] Observations in 2020 by the Subaru telescope confirmed David Vokrouhlický's 2015 Yarkovsky effect predictions.[18] The Goldstone radar observed Apophis March 3–11, 2021, helping to refine the orbit again,[19] and on March 25, 2021, the Jet Propulsion Laboratory announced that Apophis has no chance of impacting Earth in the next 100 years.[20][21] The uncertainty in the 2029 approach distance has been reduced from hundreds of kilometers to now just a couple of kilometers,[22] greatly enhancing predictions of future approaches.

Discovery and naming edit

Asteroid Apophis – closest approach to Earth on April 13, 2029[23]
(00:20; VideoFile; April 29, 2019) (turquoise dots = artificial satellites; pink = International Space Station)

Apophis was discovered on June 19, 2004, by Roy A. Tucker, David J. Tholen, and Fabrizio Bernardi at the Kitt Peak National Observatory.[1] On December 21, 2004, Apophis passed 0.0964 AU (14.42 million km; 8.96 million mi) from Earth.[1] Precovery observations from March 15, 2004, were identified on December 27, and an improved orbit solution was computed.[24][25] Radar astrometry in January 2005 further refined its orbit solution.[26][27] The discovery was notable in that it was at a very low solar elongation (56°) and at very long range (1.1 AU).[citation needed]

When first discovered, the object received the provisional designation 2004 MN4, and early news and scientific articles naturally referred to it by that name. Once its orbit was sufficiently well calculated, it received the permanent number 99942 (on June 24, 2005). Receiving a permanent number made it eligible for naming by its discoverers, and they chose the name "Apophis" on July 19, 2005.[28] Apophis is the Greek name of Apep, an enemy of the Ancient Egyptian sun-god Ra. He is the Uncreator, an evil serpent that dwells in the eternal darkness of the Duat and tries to swallow Ra during his nightly passage. Apep is held at bay by Set, the Ancient Egyptian god of storms and the desert.[29]

Tholen and Tucker, two of the co-discoverers of the asteroid, are reportedly fans of the television series Stargate SG-1. One of the show's persistent villains is an alien named Apophis. He is one of the principal threats to the existence of civilization on Earth through the first few seasons, thus likely why the asteroid was named after him. In the fictional world of the show, the alien's backstory was that he had lived on Earth during ancient times and had posed as a god, thereby giving rise to the myth of the Egyptian god of the same name.[28]

The mythological creature Apophis is pronounced with the accent on the first syllable (/ˈæpəfɪs/). In contrast, the asteroid's name is generally accented on the second syllable (/əˈpɒfɪs/) as the name was pronounced in the TV series.

Physical characteristics edit

 
Comparison between the best-fit convex and nonconvex shape models, and some of the available radar images of (99942) Apophis
 
Comparison of possible size of Apophis asteroid to Eiffel Tower and Empire State Building

Based upon the observed brightness, Apophis's diameter was initially estimated at 450 metres (1,480 ft); a more refined estimate based on spectroscopic observations at NASA's Infrared Telescope Facility in Hawaii by Binzel, Rivkin, Bus, and Tokunaga (2005) is 350 metres (1,150 ft). NASA's impact risk page lists the diameter at 330 metres (1,080 ft) and lists a mass of 4×1010 kg based on an assumed density of 2.6 g/cm3.[3] The mass estimate is more approximate than the diameter estimate, but should be accurate to within a factor of three.[3] Apophis's surface composition probably matches that of LL chondrites.[30]

Based on Goldstone and Arecibo radar images taken in 2012–2013, Brozović et al. have estimated that Apophis is an elongated object 450 × 170 metres in size, and that it is bilobed (possibly a contact binary) with a relatively bright surface albedo of 0.35±0.10. Its rotation axis has an obliquity of −59° against the ecliptic, which means that Apophis is a retrograde rotator.[2]

During the 2029 approach, Apophis's brightness will peak at magnitude 3.1,[31] easily visible to the naked eye, with a maximum angular speed of 42° per hour. The maximum apparent angular diameter will be approximately 2 arcseconds. This is roughly equivalent to the angular diameter of Neptune from earth. Therefore, the asteroid will be barely resolved by ground-based telescopes not equipped with adaptive optics but very well resolved by those that are.[32] Because the approach will be so close, tidal forces are likely to alter Apophis's rotation axis. A partial resurfacing of the asteroid is possible, which might change its spectral class from a weathered Sq- to an unweathered Q-type.[2][30]

Orbit edit

Apophis has a low inclination orbit (3.3°) that varies from just outside the orbit of Venus (0.746 AU) to just outside the orbit of Earth (1.099 AU).[1] After the 2029 Earth approach, the orbit will vary from just inside of Earth's to just inside of Mars's.

Position uncertainty and increasing divergence[1]
Date JPL SBDB
nominal geocentric
distance (AU)
uncertainty
region
(3-sigma)
2004-12-21 0.09638 AU (14.418 million km) n/a
2013-01-09 0.09666 AU (14.460 million km) n/a
2029-04-13 0.000254128 AU (38,017.0 km) ±3.4 km[22]
2036-03-27 0.309756 AU (46.3388 million km) ±130 thousand km[33]
2051-04-20 0.041455 AU (6.2016 million km) ±250 thousand km
2066-09-16 0.069562 AU (10.4063 million km) ±910 thousand km
2116-04-12 0.019462 AU (2.9115 million km) ±13 million km[34][b]
2117-10-07 0.48 AU (72 million km) ±37 million km[35]

2029 close approach edit

The closest known approach of Apophis occurs at April 13, 2029 21:46 UT, when Apophis will pass Earth closer than geosynchronous communication satellites, but will come no closer than 31,600 kilometres (19,600 mi) above Earth's surface.[36][37] Using the June 2021 orbit solution which includes the Yarkovsky effect, the 3-sigma uncertainty region in the 2029 approach distance is about ±3.4 km.[22][1] The distance, a hair's breadth in astronomical terms, is five times the radius of the Earth, ten times closer than the Moon,[37] and closer than the ring of geostationary satellites currently orbiting the Earth.[38][39] It will be the closest asteroid of its size in recorded history. On that date, it will become as bright as magnitude 3.1[31] (visible to the naked eye from rural as well as darker suburban areas, visible with binoculars from most locations).[40] The close approach will be visible from Europe, Africa, and western Asia. During the approach, Earth will perturb Apophis from an Aten-class orbit with a semi-major axis of 0.92 AU to an Apollo-class orbit with a semi-major axis of 1.1 AU.[41] Perihelion will lift from 0.746 AU to 0.895 AU and aphelion will lift from 1.10 AU to 1.31 AU.[41]

Orbital elements for 2029 (pre-flyby) and 2030 (post-flyby)[41]
Parameter Epoch Orbit
type
Orbital
period
Semi-major
axis
Perihelion Aphelion Inclination Eccentricity
Units AU (°)
Pre-flyby 2029 Aten 0.89 years (323.6 days) 0.922 0.746 1.10 3.34° 0.191
Post-flyby 2030 Apollo 1.16 years (423.1 days) 1.103 0.895 1.31 2.22° 0.189
Animation of 99942 Apophis orbit in 2028–2029
 
Around Sun
 
Around Earth
   Sun ·    Earth ·    99942 Apophis  ·    Moon
History of close approaches of large near-Earth objects since 1908 (A)
PHA Date Approach distance in lunar distances Abs. mag
(H)
Diameter (C)
(m)
Ref (D)
Nominal(B) Minimum Maximum
(152680) 1998 KJ9 1914-12-31 0.606 0.604 0.608 19.4 279–900 data
(458732) 2011 MD5 1918-09-17 0.911 0.909 0.913 17.9 556–1795 data
(163132) 2002 CU11 1925-08-30 0.903 0.901 0.905 18.5 443–477 data
69230 Hermes 1937-10-30 1.926 1.926 1.927 17.5 700-900[42] data
69230 Hermes 1942-04-26 1.651 1.651 1.651 17.5 700-900[42] data
2017 NM6 1959-07-12 1.89 1.846 1.934 18.8 580–1300 data
(27002) 1998 DV9 1975-01-31 1.762 1.761 1.762 18.1 507–1637 data
2002 NY40 2002-08-18 1.371 1.371 1.371 19.0 335–1082 data
2004 XP14 2006-07-03 1.125 1.125 1.125 19.3 292–942 data
2015 TB145 2015-10-31 1.266 1.266 1.266 20.0 620-690 data
(137108) 1999 AN10 2027-08-07 1.014 1.010 1.019 17.9 556–1793 data
(153814) 2001 WN5 2028-06-26 0.647 0.647 0.647 18.2 921–943 data
99942 Apophis 2029-04-13 0.0981 0.0963 0.1000 19.7 310–340 data
2017 MB1 2072-07-26 1.216 1.215 2.759 18.8 367–1186 data
2011 SM68 2072-10-17 1.875 1.865 1.886 19.6 254–820 data
(163132) 2002 CU11 2080-08-31 1.655 1.654 1.656 18.5 443–477 data
(416801) 1998 MZ 2116-11-26 1.068 1.068 1.069 19.2 305–986 data
(153201) 2000 WO107 2140-12-01 0.634 0.631 0.637 19.3 427–593 data
(276033) 2002 AJ129 2172-02-08 1.783 1.775 1.792 18.7 385–1242 data
(290772) 2005 VC 2198-05-05 1.951 1.791 2.134 17.6 638–2061 data
(A) This list includes near-Earth approaches of less than 2 lunar distances (LD) of objects with H brighter than 20.
(B) Nominal geocentric distance from the center of Earth to the center of the object (Earth has a radius of approximately 6,400 km).
(C) Diameter: estimated, theoretical mean-diameter based on H and albedo range between X and Y.
(D) Reference: data source from the JPL SBDB, with AU converted into LD (1 AU≈390 LD)
(E) Color codes:   unobserved at close approach   observed during close approach   upcoming approaches

2036 approaches edit

In 2036, Apophis will pass the Earth at a third the distance of the Sun in both March and December.[1] Using the 2021 orbit solution, the Earth approach on March 27, 2036, will be no closer than 0.3089 AU (46.21 million km; 28.71 million mi; 120.2 LD), but more likely about 0.3097 AU (46.33 million km; 28.79 million mi).[1] For comparison, the planet Venus will be closer to Earth at 0.2883 AU (43.13 million km; 26.80 million mi; 112.2 LD) on May 30, 2036.[43][c] On 31 December 2036 Apophis will be a little bit further away than the March approach at about 0.33 AU (49 million km; 31 million mi).

2051 approach edit

Around April 19–20, 2051, Apophis will pass about 0.04 AU (6.0 million km; 3.7 million mi) from Earth and it will be the first time since 2029 that Apophis will pass within 10 million km of Earth.[1]

2066 and 2068 edit

In the 2060s, Apophis will approach Earth in September 2066,[1][44] and then from February 2067 to December 2071, Apophis will remain farther from Earth than the Sun is.[45] On April 12, 2068, JPL Horizons calculates that Apophis will be about 1.864 ± 0.003 AU (278.85 ± 0.45 million km) from Earth,[46][15] making the asteroid much further than the Sun.

By 2116, the JPL Small-Body Database and NEODyS close approach data start to become divergent.[1][44] In April 2116, Apophis is expected to pass about 0.02 AU (3 million km; 8 LD) from Earth, but could pass as close as 0.001 AU (150 thousand km; 0.39 LD) or could pass as far as 0.1 AU (15 million km; 39 LD).[1]

Refinement of close approach predictions edit

Six months after discovery, and shortly after a close approach to Earth on December 21, 2004, the improved orbital estimates led to the prediction of a very close approach on April 13, 2029, by both NASA's automatic Sentry system and NEODyS, a similar automatic program run by the University of Pisa and the University of Valladolid. Subsequent observations decreased the uncertainty in Apophis's trajectory. The probability of an impact event in 2029 temporarily climbed, peaking at 2.7% (1 in 37) on December 27, 2004,[47][48] when the uncertainty region had shrunk to 83,000 km.[49] This probability, combined with its size, caused Apophis to be assessed at level 4 on the Torino scale[13] and 1.10 on the Palermo Technical Impact Hazard Scale, scales scientists use to represent how dangerous a given asteroid is to Earth. These are the highest values for which any object has been rated on either scale. The chance that there would be an impact in 2029 was eliminated by late December 27, 2004, as a result of a precovery image that extended the observation arc back to March 2004.[25] The danger of a 2036 passage was lowered to level 0 on the Torino scale in August 2006.[50] With a cumulative Palermo Scale rating of −3.22,[3] the risk of impact from Apophis is less than one thousandth the background hazard level.[3]

2005 and 2011 observations edit

In July 2005, former Apollo astronaut Rusty Schweickart, as chairman of the B612 Foundation, formally asked NASA to investigate the possibility that the asteroid's post-2029 orbit could be in orbital resonance with Earth, which would increase the probability of future impacts. Schweickart also asked NASA to investigate whether a transponder should be placed on the asteroid to enable more accurate tracking of how its orbit is affected by the Yarkovsky effect.[51] On January 31, 2011, astronomers took the first new images of Apophis in more than 3 years.[52]

 
Illustration of a common trend where progressively reduced uncertainty regions result in an asteroid impact probability increasing followed by a sharp decrease

2013 refinement edit

The close approach in 2029 will substantially alter the object's orbit, prompting Jon Giorgini of JPL to say in 2011, "If we get radar ranging in 2013 [the next good opportunity], we should be able to predict the location of 2004 MN4 out to at least 2070."[53] Apophis passed within 0.0966 AU (14.45 million km; 8.98 million mi) of Earth in 2013, allowing astronomers to refine the trajectory for future close passes.[9][44][54] Just after the closest approach on January 9, 2013,[44] the asteroid peaked at an apparent magnitude of about 15.6.[55] The Goldstone radar observed Apophis during that approach from January 3 through January 17.[56] The Arecibo Observatory observed Apophis once it entered Arecibo's declination window after February 13, 2013.[56] The 2013 observations basically ruled out any chance of a 2036 impact.

A NASA assessment as of February 21, 2013, that did not use the January and February 2013 radar measurements gave an impact probability of 2.3 in a million for 2068.[57] As of May 6, 2013, using observations through April 15, 2013, the odds of an impact on April 12, 2068, as calculated by the JPL Sentry risk table had increased slightly to 3.9 in a million (1 in 256,000).[3]

2015 observations edit

As of January 2019, Apophis had not been observed since 2015, mostly because its orbit kept it very near the Sun from the perspective of Earth. It was not further than 60 degrees from the Sun between April 2014 and December 2019. With the early 2015 observations, the April 12, 2068, impact probability was 6.7 in a million (1 in 150,000), and the asteroid had a cumulative 9 in a million (1 in 110,000) chance of impacting Earth before 2106.[58]

2020–21 observations edit

Apophis in February 2021

No observations of Apophis were made between January 2015 and February 2019, and then observations started occurring regularly in January 2020.[59] In March 2020, astronomers David Tholen and Davide Farnocchia measured the acceleration of Apophis due to the Yarkovsky effect for the first time, significantly improving the prediction of its orbit past the 2029 flyby. Tholen and Farnocchia found that the Yarkovsky effect caused Apophis to drift by about 170 meters per year.[60] In late 2020, Apophis approached the Earth again. It passed 0.11265 AU (16.852 million km; 43.84 LD) from Earth on March 6, 2021, brightening to +15 mag at the time. Radar observations of Apophis were planned at Goldstone in March 2021.[19] The asteroid has been observed by NEOWISE (between December 2020 and April 2021)[61][62] and by NEOSSat (in January 2021).[6][63][7] Apophis was the target of an observing campaign by IAWN, resulting in the collection of light curves, spectra, and astrometry.[6][63][7] The observations were used to practice and coordinate the response to an actual impact threat.[64]

 
Hypothetical risk corridor for an impact on 13 April 2029, based on the 2020–21 planetary defense exercise

On February 21, 2021, Apophis was removed from the Sentry Risk Table, as an impact in the next 100 years was finally ruled out.[65]

Several occultations of bright stars (apparent magnitude 8–11) by Apophis occurred in March and April 2021.[66][67][68][69] A total of five separate occultations were observed successfully, marking the first time that an asteroid as small as Apophis was observed using the occultation method (beating the previous record set in 2019 by asteroid 3200 Phaeton by more than a factor of ten).[67] The first event, on March 7, was successfully observed from the United States by multiple observers.[70][71][66] The next potential occultation, which occurred on March 11, was predicted to be visible from central Europe.[68] This event was missed, mainly because of bad weather (two negative observations were recorded from Greece).[67] On March 22, another occultation was observed only by a single observer from the United States, amateur astronomer Roger Venable. Larger-than-expected residuals in the March 7 data had caused the majority of observers to be deployed outside of the actual path for the March 22 occultation.[66] This single detection then allowed the prediction of several more events that would have been unobservable otherwise, including an occultation on April 4, which was observed from New Mexico, again by Venable, alongside others.[69][66] Two more occultations, observable on April 10 and April 11 from Japan and New Mexico, respectively, were seen by several observers each.[66]

On March 9, 2021, using radar observations from Goldstone taken on March 3–8 and three positive detections of the stellar occultation on March 7, 2021,[72] Apophis became the asteroid with the most precisely measured Yarkovsky effect of all asteroids, at a signal-to-noise ratio (SNR) of 186.4,[73][d] surpassing 101955 Bennu (SNR=181.6).[74]

The 2021 apparition was the last opportunity to observe Apophis before its 2029 flyby.[1]

 
Asteroid 99942 Apophis – radar observations March 8–10, 2021 (March 26, 2021)

History of impact estimates edit

Date Time Status
2004-12-23 The original NASA report mentioned impact chances of "around 1 in 300" in 2029, which was widely reported in the media.[13] The actual NASA estimates at the time were 1 in 233; these resulted in a Torino scale rating of 2, the first time any asteroid had received a rating above 1.
Later that day, based on a total of 64 observations, the estimates were changed to 1 in 62 (1.6%), resulting in an update to the initial report and an upgrade to a Torino scale rating of 4.
2004-12-25 The chances were first reported as 1 in 42 (2.4%) and later that day (based on 101 observations) as 1 in 45 (2.2%). At the same time, the asteroid's estimated diameter was lowered from 440 m to 390 m and its mass from 1.2×1011 kg to 8.3×1010 kg.
2004-12-26 Based on a total of 169 observations, the impact probability was still estimated as 1 in 45 (2.2%), the estimates for diameter and mass were lowered to 380 m and 7.5×1010 kg, respectively.
2004-12-27 Based on a total of 176 observations with an observation arc of 190 days, the impact probability was raised to 1 in 37 (2.7%)[48] with a line of variation (LOV) of only 83,000 km;[49] diameter was increased to 390 m, and mass to 7.9×1010 kg.
Later that afternoon, a precovery increased the span of observations to 287 days, which eliminated the 2029 impact threat.[25] The cumulative impact probability was estimated to be around 0.004%, a risk lower than that of asteroid 2004 VD17, which once again became the greatest-risk object. A 2053 approach to Earth still poses a minor risk of impact, and Apophis was still rated at level one on the Torino scale for this orbit.
2004-12-28 12:23 GMT Based on a total of 139 observations, a value of one was given on the Torino scale for 2044-04-13.29 and 2053-04-13.51.
2004-12-29 01:10 GMT The only pass rated 1 on the Torino scale was for 2053-04-13.51 based on 139 observations spanning 287.71 days (2004-Mar-15.1104 to 2004-Dec-27.8243). (As of February 2013 the 2053 risk is only 1 in 20 billion.)[3]
19:18 GMT This was still the case based upon 147 observations spanning 288.92 days (2004-Mar-15.1104 to 2004-Dec-29.02821), though the close encounters have changed and been reduced to 4 in total.
2004-12-30 13:46 GMT No passes were rated above 0, based upon 157 observations spanning 289.33 days (2004-Mar-15.1104 to 2004-Dec-29.44434). The most dangerous pass was rated at 1 in 7,143,000.
22:34 GMT 157 observations spanning 289.33 days (2004-Mar-15.1104 to 2004-Dec-29.44434). One pass at 1 (Torino scale) 3 other passes.
2005-01-02 03:57 GMT Observations spanning 290.97 days (2004-Mar-15.1104 to 2004-Dec-31.07992) One pass at 1 (Torino scale) 19 other passes.
2005-01-03 14:49 GMT Observations spanning 292.72 days (2004-Mar-15.1104 to 2005-Jan-01.82787) One pass at 1 (Torino scale) 15 other passes.
2005–01 Extremely precise radar observations at Arecibo Observatory[26] refine the orbit further and show that the April 2029 close approach will occur at only 5.7 Earth radii,[27] approximately one-half the distance previously estimated.
2005-02-06 Apophis (2004 MN4) had a 1-in-13,000 chance of impacting in April 2036.[75]
2005-08-07 Radar observation[26] refines the orbit further and eliminates the possibility of an impact in 2035. Only the pass in 2036 remains at Torino scale 1 (with a 1-in-5,560 chance of impact).[76]
2005–10 It is predicted that Apophis will pass just below the altitude of geosynchronous satellites, which are at approximately 35,900 kilometres (22,300 mi).[77] Such a close approach by an asteroid of that size is estimated to occur every 800 years or so.[78]
2006-05-06 Radar observation at Arecibo Observatory[26] slightly lowered the Palermo scale rating, but the pass in 2036 remained at Torino scale 1[79] despite the impact probability dropping by a factor of four.
2006-08-05 Additional observations through 2006 resulted in Apophis being lowered to Torino scale 0.[50] (The impact probability was 1 in 45,000.)[50]
2008-04 Nico Marquardt published a research paper in which he calculated the probability of Apophis to collide with a geosynchronous satellite during its flyby on April 13, 2029, and the consequences of this event to the likelihood of an Earth-collision 2036. Afterwards, the German newspaper Bild published an article stating a 100 times higher probability of an Earth-collision in the year 2036 than Marquardt calculated.[80] Nearly all international press reported the news with false data caused by the review from Bild even though Marquardt denied.[81] This estimate was allegedly confirmed by ESA and NASA[82][80] but in an official statement,[83] NASA denied the wrong statement. The release went on to explain that since the angle of Apophis's approach to the Earth's equator means the asteroid will not travel through the belt of current equatorial geosynchronous satellites, there is currently no risk of collision; and the effect on Apophis's orbit of any such impact would be insignificant.
2008-04-16 NASA News Release 08-103 reaffirmed that its estimation of a 1-in-45,000 chance of impact in 2036 remained valid.[83]
2009-04-29 An animation is released[84] that shows how unmeasured physical parameters of Apophis bias the entire statistical uncertainty region. If Apophis is a retrograde rotator on the small, less-massive end of what is possible, the measurement uncertainty region will get pushed back such that the center of the distribution encounters Earth's orbit. This would result in an impact probability much higher than computed with the Standard Dynamical Model. Conversely, if Apophis is a small, less-massive prograde rotator, the uncertainty region is advanced along the orbit. Only the remote tails of the probability distribution could encounter Earth, producing a negligible impact probability.
2009-10-07 Refinements to the precovery images of Apophis by the University of Hawaii's Institute for Astronomy, the 90-inch Bok Telescope, and the Arecibo Observatory have generated a refined path that reduces the odds of an April 13, 2036, impact to about 1 in 250,000.[85]
Criticism of older published impact probabilities rests on the fact that important physical parameters such as mass and spin that affect its precise trajectory have not yet been accurately measured and hence there are no associated probability distributions. The Standard Dynamical Model used for making predictions simplifies calculations by assuming Earth is a point mass; this can introduce up to 2.9 Earth radii of prediction error for the 2036 approach, and Earth's oblateness must be considered for the 2029 passage to predict a potential impact reliably.[78] Additional factors that can greatly influence the predicted motion in ways that depend on unknown details, are the spin of the asteroid,[86] its precise mass, the way it reflects and absorbs sunlight, radiates heat, and the gravitational pull of other asteroids passing nearby.[78] Small uncertainties in the masses and positions of the planets and Sun can cause up to 23 Earth radii of prediction error for Apophis by 2036.[78]
2013-01 A statistical impact risk analysis of the data up to this point calculated that the odds of the 2036 impact at 7.07 in a billion, effectively ruling it out. The same study looked at the odds of an impact in 2068, which were calculated at 2.27 in a million.[87] First appearance of Sentry virtual impactors that also include mid-October dates.[88]
2013-01-09 The European Space Agency (ESA) announced the Herschel Space Observatory made new thermal infrared observations of the asteroid as it approached Earth. The initial data shows the asteroid to be bigger than first estimated because it is now expected to be less reflective than originally thought.[9] The Herschel Space Observatory observations increased the diameter estimate by 20% from 270 to 325 metres, which translates into a 75% increase in the estimates of the asteroid's volume or mass.[9] Goldstone single-pixel observations of Apophis have ruled out the potential 2036 Earth impact.[14][89][90] Apophis will then come no closer than about 23 million kilometres (14×10^6 mi)—and more likely miss us by something closer to 56 million kilometres (35×10^6 mi).[89] The radar astrometry is more precise than was expected.[89]
2016-03-25 The Sentry Risk Table assessed Apophis as having a 6.7-in-a-million (1-in-150,000) chance of impacting Earth in 2068, and a 9-in-a-million (1-in-110,000) cumulative chance of impacting Earth by 2105.[3]
2020-03 By taking observations of Apophis with the Subaru Telescope in January and March 2020, as well as remeasuring older observations using the new Gaia DR2 star catalog, astronomers positively detect the Yarkovsky effect on Apophis. The asteroid's position is found to shift by 170 meters per year. The Yarkovsky effect is the main source of uncertainty in impact probability estimates for this asteroid.[60]
2021-01-20 The Sentry Risk Table assessed Apophis as having a 2.6-in-a-million (1-in-380,000) chance of impacting Earth in 2068, and a 4.5-in-a-million (1-in-220,000) cumulative chance of impacting Earth by 2107.[3] The previous 2068 odds were 1-in-150,000.
2021-03-15 10:44 JPL solution #207 using observations in 2020 and 2021 reduced the 3-sigma uncertainty region in the 2029 approach distance from ±700 km[91] to about ±3 km.[1] The June 2021 solution showed the Earth approach on March 27, 2036, will be no closer than 0.30889 AU (46.209 million km; 28.713 million mi; 120.21 LD).[1]

Possible impact effects edit

The Sentry Risk Table estimates that Apophis would impact Earth with kinetic energy equivalent to 1,200 megatons of TNT. In comparison, the Chicxulub impact which caused the mass extinction event responsible for wiping out the dinosaurs has been estimated to have released about as much energy as 100,000,000 megatons (100 teratons). The exact effects of any impact would vary based on the asteroid's composition, and the location and angle of impact. Any impact would be extremely detrimental to an area of thousands of square kilometres, but would be unlikely to have long-lasting global effects, such as the initiation of an impact winter.[citation needed] Assuming Apophis is a 370-metre-wide (1,210 ft) stony asteroid with a density of 3,000 kg/m3, if it were to impact into sedimentary rock, Apophis would create a 5.1-kilometre (17,000 ft) impact crater.[17][3]

Expired 2036 path of risk edit

In 2008, the B612 Foundation made estimates of Apophis's path if a 2036 Earth impact were to occur, as part of an effort to develop viable deflection strategies.[92] The result was a narrow corridor a few kilometres wide, called the "path of risk", extending across southern Russia, across the north Pacific (relatively close to the coastlines of California and Mexico), then right between Nicaragua and Costa Rica, crossing northern Colombia and Venezuela, ending in the Atlantic, just before reaching Africa.[93] Using the computer simulation tool NEOSim, it was estimated that the hypothetical impact of Apophis in countries such as Colombia and Venezuela, which were in the path of risk, could have more than 10 million casualties.[94] A deep-water impact in the Atlantic or Pacific oceans would produce an incoherent short-range tsunami with a potential destructive radius (inundation height of >2 m) of roughly 1,000 kilometres (620 mi) for most of North America, Brazil and Africa, 3,000 km (1,900 mi) for Japan and 4,500 km (2,800 mi) for some areas in Hawaii.[95]

Exploration edit

OSIRIS-APEX post-Earth-encounter rendezvous edit

The OSIRIS-REx spacecraft returned a sample of Bennu to Earth on 24 September 2023.[96] After ejecting the sample canister, the spacecraft can use its remaining fuel to target another body during an extended mission. Apophis is the only asteroid which the spacecraft could reach for a long-duration rendezvous, rather than a brief flyby. In April 2022, the extension was approved, and OSIRIS-REx will perform a rendezvous with Apophis in April 2029, a few days after the close approach to Earth. It will study the asteroid for 18 months and perform a maneuver similar to the one it made during sample collection at Bennu, by approaching the surface and firing its thrusters. This will expose the asteroid's subsurface and allow mission scientists to learn more about the asteroid's material properties.[97][98] For its Apophis mission after the sample return, OSIRIS-REx was renamed OSIRIS-APEX (short for OSIRIS-Apophis Explorer).[99]

Other proposed space missions edit

Planetary Society competition edit

In 2007, The Planetary Society, a California-based space advocacy group, organized a $50,000 competition to design an uncrewed space probe that would 'shadow' Apophis for almost a year, taking measurements that would "determine whether it will impact Earth, thus helping governments decide whether to mount a deflection mission to alter its orbit". The society received 37 entries from 20 countries on 6 continents.

The commercial competition was won by a design called 'Foresight' created by SpaceWorks Enterprises, Inc.[100] SpaceWorks proposed a simple orbiter with only two instruments and a radio beacon at a cost of ~US$140 million, launched aboard a Minotaur IV between 2012 and 2014, to arrive at Apophis five to ten months later. It would then rendezvous with, observe, and track the asteroid. Foresight would orbit the asteroid to gather data with a multi-spectral imager for one month. It would then leave orbit and fly in formation with Apophis around the Sun at a range of two kilometres (1.2 miles). The spacecraft would use laser ranging to the asteroid and radio tracking from Earth for ten months to accurately determine the asteroid's orbit and how it might change.

Pharos, the winning student entry, would be an orbiter with four science instruments (a multi-spectral imager, near-infrared spectrometer, laser rangefinder, and magnetometer) that would rendezvous with and track Apophis. Earth-based tracking of the spacecraft would then allow precise tracking of the asteroid. The Pharos spacecraft would also carry four instrumented probes that it would launch individually over the course of two weeks. Accelerometers and temperature sensors on the probes would measure the seismic effects of successive probe impacts, a creative way to explore the interior structure and dynamics of the asteroid.

Second place, for $10,000, went to a European team led by Deimos Space S.L. of Madrid, Spain, in cooperation with EADS Astrium, Friedrichshafen, Germany; University of Stuttgart, Germany; and University of Pisa, Italy. Juan L. Cano was principal investigator.

Another European team took home $5,000 for third place. Their team lead was EADS Astrium Ltd, United Kingdom, in conjunction with EADS Astrium SAS, France; IASF-Roma, INAF, Rome, Italy; Open University, UK; Rheinisches Institut für Umweltforschung, Germany; Royal Observatory of Belgium; and Telespazio, Italy. The principal investigator was Paolo D'Arrigo.

Two teams tied for second place in the Student Category: Monash University, Clayton Campus, Australia, with Dilani Kahawala as principal investigator; and University of Michigan, with Jeremy Hollander as principal investigator. Each second-place team won $2,000. A team from Hong Kong Polytechnic University and Hong Kong University of Science and Technology, under the leadership of Peter Weiss, received an honorable mention and $1,000 for the most innovative student proposal.

Don Quijote mission edit

Apophis is one of two asteroids that were considered by the European Space Agency as the target of its Don Quijote mission concept to study the effects of impacting an asteroid.[101]

Cancelled Chinese mission edit

China had planned an encounter with Apophis in 2022, several years prior to the close approach in 2029. This mission, now known as Tianwen-2, would have included exploration and close study of three asteroids including an extended encounter with Apophis for close observation, and land on the asteroid 1996 FG3 to conduct in situ sampling analysis on the surface.[102] The launch date is now scheduled for 2024, with a different set of targets.

RAMSES edit

Apophis is the target of the European Space Agency's proposed RAMSES (Rapid Apophis Mission for SEcurity and Safety) mission, with a launch in 2027 and rendezvous with the asteroid in 2029.[103]

Proposed deflection strategies edit

Studies by NASA, ESA,[104] and various research groups in addition to the Planetary Society contest teams,[105] have described a number of proposals for deflecting Apophis or similar objects, including gravitational tractor, kinetic impact, and nuclear bomb methods.

On December 30, 2009, Anatoly Perminov, the director of the Russian Federal Space Agency, said in an interview that Roscosmos will also study designs for a possible deflection mission to Apophis.[106]

On August 16, 2011, researchers at China's Tsinghua University proposed launching a mission to knock Apophis onto a safer course using an impactor spacecraft in a retrograde orbit, steered and powered by a solar sail. Instead of moving the asteroid on its potential resonant return to Earth, Shengping Gong and his team believe the secret is shifting the asteroid away from entering the gravitational keyhole in the first place.[107]

On February 15, 2016, Sabit Saitgarayev, of the Makeyev Rocket Design Bureau, announced intentions to use Russian ICBMs to target relatively small near-Earth objects. Although the report stated that likely targets would be between the 20 to 50 metres in size, it was also stated that 99942 Apophis would be an object subject to tests by the program.[108]

In October 2022, a method of mapping the inside of a potentially problematic asteroid, such as 99942 Apophis, in order to determine the best area for impact was proposed.[109]

Popular culture edit

In Id Software's video game Rage, the backstory involves the asteroid colliding with Earth on August 23, 2029. The asteroid almost wipes out the human race and ushers in a post-apocalyptic age.[110]

See also edit

Notes edit

  1. ^ Of the six asteroids with a riskier palermo scale rating than Apophis:
  2. ^ The minimum possible Earth approach between 5–20 April 2116 is 0.001 AU (150 thousand km; 93 thousand mi; 0.39 LD).
  3. ^ On January 8, 2022 Venus was even closer to Earth at 0.2658 AU (39.76 million km; 24.71 million mi; 103.4 LD).
  4. ^ Using the 9 March 2021 solution, JPL gave the strength of the Yarkovsky effect as  , with an uncertainty of  . The SNR, defined as the size of the signal divided by the uncertainty, is  . As of the latest orbit solution (29 June 2021), the SNR is   (again lower than Bennu's).

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External links edit

  • Müller, T. G.; Kiss, C.; Scheirich, P.; Pravec, P.; et al. (2014). "Thermal infrared observations of asteroid (99942) Apophis with Herschel". Astronomy & Astrophysics. 566: A22. arXiv:1404.5847. Bibcode:2014A&A...566A..22M. doi:10.1051/0004-6361/201423841. S2CID 119282830.
  • Asteroid Apophis orbit from recent observations, EPSC Abstracts Vol. 6, EPSC-DPS2011-1212, 2011, EPSC-DPS Joint Meeting 2011
  • Diagrams and orbits of Apophis (Sormano Astronomical Observatory)

Risk assessment

  • Apophis Orbital Prediction Page at NASA JPL
  • 99942 Apophis page from NEODyS
  • MBPL – Minor Body Priority List (technical List) at Sormano Observatory
  • TECA – Table of Asteroids Next Closest Approaches to the Earth at Sormano Observatory

NASA

  • (JPL)
  • Radar Observations Refine the Future Motion of Asteroid 2004 MN4 (JPL)
  • from
  • 99942 Apophis at the JPL Small-Body Database
    • Close approach · Discovery · Ephemeris · Orbit diagram · Orbital elements · Physical parameters
Preceded by Large NEO Earth close approach
(inside the orbit of the Moon)

13 April 2029
Succeeded by

99942, apophis, provisional, designation, 2004, near, earth, asteroid, potentially, hazardous, object, with, diameter, metres, feet, that, caused, brief, period, concern, december, 2004, when, initial, observations, indicated, probability, that, would, earth, . 99942 Apophis provisional designation 2004 MN4 is a near Earth asteroid and a potentially hazardous object with a diameter of 370 metres 1 210 feet 3 that caused a brief period of concern in December 2004 when initial observations indicated a probability up to 2 7 that it would hit Earth on April 13 2029 Additional observations provided improved predictions that eliminated the possibility of an impact on Earth in 2029 Until 2006 a small possibility nevertheless remained that during its 2029 close encounter with Earth Apophis would pass through a gravitational keyhole of no more than about 800 kilometres 500 mi in diameter 11 12 which would have set up a future impact exactly seven years later on April 13 2036 This possibility kept it at Level 1 on the Torino impact hazard scale until August 2006 when the probability that Apophis would pass through the keyhole was determined to be very small and Apophis s rating on the Torino scale was lowered to zero By 2008 the keyhole had been determined to be less than 1 km wide 11 During the short time when it had been of greatest concern Apophis set the record for highest rating ever on the Torino scale reaching level 4 on December 27 2004 13 99942 ApophisModel of 99942 Apophis s shape assuming the entire surface is of a similar composition Discovery 1 Discovered byRoy A TuckerDavid J TholenFabrizio BernardiDiscovery siteKitt Peak 1 Discovery dateJune 19 2004DesignationsMPC designation 99942 ApophisPronunciation e ˈ p ɒ f e s trad ˈ ae p e f e s Named afterἌpofis ApophisAlternative designations2004 MN4Minor planet categoryAtenNEOPHA 1 AdjectivesApophidian ae p e ˈ f ɪ d i e n Latin Apŏpidis Orbital characteristics 1 Epoch 13 September 2023 JD 2453300 5 Uncertainty parameter 0Observation arc6267 days 17 16 yr Earliest precovery dateMarch 15 2004Aphelion1 0994 AU 164 47 million km Perihelion0 7461 AU 111 61 million km Semi major axis0 9227 AU 138 03 million km Eccentricity0 19144Orbital period sidereal 0 89 yr 323 7 d Average orbital speed30 73 km sMean anomaly142 9 Mean motion1 11198 dayInclination3 339 Longitude of ascending node203 96 Argument of perihelion126 60 Earth MOID0 00026 AU 39 thousand km Jupiter MOID4 12 AU 616 million km TJupiter6 464Physical characteristicsDimensions0 370 km 0 230 mi 0 45 0 17 km 2 Mean radius0 185 km 0 115 mi 0 17 0 02 km 2 Mass6 1 1010 kg assumed 3 Mean density 3 2 g cm3 4 2 6 g cm3 assumed 3 Synodic rotation period30 4 h 1 27 d 1 5 30 55 0 12 h 6 30 67 0 06 h 7 Tumbling 8 27 38 0 07 h precession period 8 263 6 h rotation period 8 30 56 0 01 h period of harmonic with strongest lightcurve amplitude 8 Geometric albedo0 23 9 0 35 0 10 2 Temperature270 KSpectral typeSq 5 Absolute magnitude H 19 7 0 4 1 5 19 09 0 19 2 18 95 0 15 10 Preliminary observations by Goldstone radar in January 2013 effectively ruled out the possibility of an Earth impact by Apophis in 2036 14 By May 6 2013 April 15 2013 observation arc the possibility of an impact on April 13 2036 had been eliminated altogether 3 In 2036 Apophis will approach the Earth at a third the distance of the Sun in both March and December 1 but this is about the distance of the planet Venus when it overtakes Earth every 1 6 years On April 12 2068 the nominal trajectory has Apophis 1 87 AU 280 million km from Earth 15 Entering March 2021 six asteroids each had a more notable cumulative Palermo Technical Impact Hazard Scale rating than Apophis and none of those has a Torino level above 0 16 a On average an asteroid the size of Apophis 370 metres is expected to impact Earth once in about 80 000 years 17 Observations in 2020 by the Subaru telescope confirmed David Vokrouhlicky s 2015 Yarkovsky effect predictions 18 The Goldstone radar observed Apophis March 3 11 2021 helping to refine the orbit again 19 and on March 25 2021 the Jet Propulsion Laboratory announced that Apophis has no chance of impacting Earth in the next 100 years 20 21 The uncertainty in the 2029 approach distance has been reduced from hundreds of kilometers to now just a couple of kilometers 22 greatly enhancing predictions of future approaches Contents 1 Discovery and naming 2 Physical characteristics 3 Orbit 3 1 2029 close approach 3 2 2036 approaches 3 3 2051 approach 3 4 2066 and 2068 3 5 Refinement of close approach predictions 3 5 1 2005 and 2011 observations 3 5 2 2013 refinement 3 5 3 2015 observations 3 5 4 2020 21 observations 3 6 History of impact estimates 4 Possible impact effects 4 1 Expired 2036 path of risk 5 Exploration 5 1 OSIRIS APEX post Earth encounter rendezvous 5 2 Other proposed space missions 5 2 1 Planetary Society competition 5 2 2 Don Quijote mission 5 2 3 Cancelled Chinese mission 5 2 4 RAMSES 6 Proposed deflection strategies 7 Popular culture 8 See also 9 Notes 10 References 11 External linksDiscovery and naming edit source source source source source source source track Asteroid Apophis closest approach to Earth on April 13 2029 23 00 20 VideoFile April 29 2019 turquoise dots artificial satellites pink International Space Station Apophis was discovered on June 19 2004 by Roy A Tucker David J Tholen and Fabrizio Bernardi at the Kitt Peak National Observatory 1 On December 21 2004 Apophis passed 0 0964 AU 14 42 million km 8 96 million mi from Earth 1 Precovery observations from March 15 2004 were identified on December 27 and an improved orbit solution was computed 24 25 Radar astrometry in January 2005 further refined its orbit solution 26 27 The discovery was notable in that it was at a very low solar elongation 56 and at very long range 1 1 AU citation needed When first discovered the object received the provisional designation 2004 MN4 and early news and scientific articles naturally referred to it by that name Once its orbit was sufficiently well calculated it received the permanent number 99942 on June 24 2005 Receiving a permanent number made it eligible for naming by its discoverers and they chose the name Apophis on July 19 2005 28 Apophis is the Greek name of Apep an enemy of the Ancient Egyptian sun god Ra He is the Uncreator an evil serpent that dwells in the eternal darkness of the Duat and tries to swallow Ra during his nightly passage Apep is held at bay by Set the Ancient Egyptian god of storms and the desert 29 Tholen and Tucker two of the co discoverers of the asteroid are reportedly fans of the television series Stargate SG 1 One of the show s persistent villains is an alien named Apophis He is one of the principal threats to the existence of civilization on Earth through the first few seasons thus likely why the asteroid was named after him In the fictional world of the show the alien s backstory was that he had lived on Earth during ancient times and had posed as a god thereby giving rise to the myth of the Egyptian god of the same name 28 The mythological creature Apophis is pronounced with the accent on the first syllable ˈaepefɪs In contrast the asteroid s name is generally accented on the second syllable eˈpɒfɪs as the name was pronounced in the TV series Physical characteristics edit nbsp Comparison between the best fit convex and nonconvex shape models and some of the available radar images of 99942 Apophis nbsp Comparison of possible size of Apophis asteroid to Eiffel Tower and Empire State BuildingBased upon the observed brightness Apophis s diameter was initially estimated at 450 metres 1 480 ft a more refined estimate based on spectroscopic observations at NASA s Infrared Telescope Facility in Hawaii by Binzel Rivkin Bus and Tokunaga 2005 is 350 metres 1 150 ft NASA s impact risk page lists the diameter at 330 metres 1 080 ft and lists a mass of 4 1010 kg based on an assumed density of 2 6 g cm3 3 The mass estimate is more approximate than the diameter estimate but should be accurate to within a factor of three 3 Apophis s surface composition probably matches that of LL chondrites 30 Based on Goldstone and Arecibo radar images taken in 2012 2013 Brozovic et al have estimated that Apophis is an elongated object 450 170 metres in size and that it is bilobed possibly a contact binary with a relatively bright surface albedo of 0 35 0 10 Its rotation axis has an obliquity of 59 against the ecliptic which means that Apophis is a retrograde rotator 2 During the 2029 approach Apophis s brightness will peak at magnitude 3 1 31 easily visible to the naked eye with a maximum angular speed of 42 per hour The maximum apparent angular diameter will be approximately 2 arcseconds This is roughly equivalent to the angular diameter of Neptune from earth Therefore the asteroid will be barely resolved by ground based telescopes not equipped with adaptive optics but very well resolved by those that are 32 Because the approach will be so close tidal forces are likely to alter Apophis s rotation axis A partial resurfacing of the asteroid is possible which might change its spectral class from a weathered Sq to an unweathered Q type 2 30 Orbit editApophis has a low inclination orbit 3 3 that varies from just outside the orbit of Venus 0 746 AU to just outside the orbit of Earth 1 099 AU 1 After the 2029 Earth approach the orbit will vary from just inside of Earth s to just inside of Mars s Position uncertainty and increasing divergence 1 Date JPL SBDBnominal geocentricdistance AU uncertaintyregion 3 sigma 2004 12 21 0 09638 AU 14 418 million km n a2013 01 09 0 09666 AU 14 460 million km n a2029 04 13 0 000254128 AU 38 017 0 km 3 4 km 22 2036 03 27 0 309756 AU 46 3388 million km 130 thousand km 33 2051 04 20 0 041455 AU 6 2016 million km 250 thousand km2066 09 16 0 069562 AU 10 4063 million km 910 thousand km2116 04 12 0 019462 AU 2 9115 million km 13 million km 34 b 2117 10 07 0 48 AU 72 million km 37 million km 35 2029 close approach edit The closest known approach of Apophis occurs at April 13 2029 21 46 UT when Apophis will pass Earth closer than geosynchronous communication satellites but will come no closer than 31 600 kilometres 19 600 mi above Earth s surface 36 37 Using the June 2021 orbit solution which includes the Yarkovsky effect the 3 sigma uncertainty region in the 2029 approach distance is about 3 4 km 22 1 The distance a hair s breadth in astronomical terms is five times the radius of the Earth ten times closer than the Moon 37 and closer than the ring of geostationary satellites currently orbiting the Earth 38 39 It will be the closest asteroid of its size in recorded history On that date it will become as bright as magnitude 3 1 31 visible to the naked eye from rural as well as darker suburban areas visible with binoculars from most locations 40 The close approach will be visible from Europe Africa and western Asia During the approach Earth will perturb Apophis from an Aten class orbit with a semi major axis of 0 92 AU to an Apollo class orbit with a semi major axis of 1 1 AU 41 Perihelion will lift from 0 746 AU to 0 895 AU and aphelion will lift from 1 10 AU to 1 31 AU 41 Orbital elements for 2029 pre flyby and 2030 post flyby 41 Parameter Epoch Orbittype Orbitalperiod Semi majoraxis Perihelion Aphelion Inclination EccentricityUnits AU Pre flyby 2029 Aten 0 89 years 323 6 days 0 922 0 746 1 10 3 34 0 191Post flyby 2030 Apollo 1 16 years 423 1 days 1 103 0 895 1 31 2 22 0 189Animation of 99942 Apophis orbit in 2028 2029 nbsp Around Sun nbsp Around Earth Sun Earth 99942 Apophis Moon History of close approaches of large near Earth objects since 1908 A PHA Date Approach distance in lunar distances Abs mag H Diameter C m Ref D Nominal B Minimum Maximum 152680 1998 KJ9 1914 12 31 0 606 0 604 0 608 19 4 279 900 data 458732 2011 MD5 1918 09 17 0 911 0 909 0 913 17 9 556 1795 data 163132 2002 CU11 1925 08 30 0 903 0 901 0 905 18 5 443 477 data69230 Hermes 1937 10 30 1 926 1 926 1 927 17 5 700 900 42 data69230 Hermes 1942 04 26 1 651 1 651 1 651 17 5 700 900 42 data2017 NM6 1959 07 12 1 89 1 846 1 934 18 8 580 1300 data 27002 1998 DV9 1975 01 31 1 762 1 761 1 762 18 1 507 1637 data2002 NY40 2002 08 18 1 371 1 371 1 371 19 0 335 1082 data2004 XP14 2006 07 03 1 125 1 125 1 125 19 3 292 942 data2015 TB145 2015 10 31 1 266 1 266 1 266 20 0 620 690 data 137108 1999 AN10 2027 08 07 1 014 1 010 1 019 17 9 556 1793 data 153814 2001 WN5 2028 06 26 0 647 0 647 0 647 18 2 921 943 data99942 Apophis 2029 04 13 0 0981 0 0963 0 1000 19 7 310 340 data2017 MB1 2072 07 26 1 216 1 215 2 759 18 8 367 1186 data2011 SM68 2072 10 17 1 875 1 865 1 886 19 6 254 820 data 163132 2002 CU11 2080 08 31 1 655 1 654 1 656 18 5 443 477 data 416801 1998 MZ 2116 11 26 1 068 1 068 1 069 19 2 305 986 data 153201 2000 WO107 2140 12 01 0 634 0 631 0 637 19 3 427 593 data 276033 2002 AJ129 2172 02 08 1 783 1 775 1 792 18 7 385 1242 data 290772 2005 VC 2198 05 05 1 951 1 791 2 134 17 6 638 2061 data A This list includes near Earth approaches of less than 2 lunar distances LD of objects with H brighter than 20 B Nominal geocentric distance from the center of Earth to the center of the object Earth has a radius of approximately 6 400 km C Diameter estimated theoretical mean diameter based on H and albedo range between X and Y D Reference data source from the JPL SBDB with AU converted into LD 1 AU 390 LD E Color codes unobserved at close approach observed during close approach upcoming approaches 2036 approaches edit In 2036 Apophis will pass the Earth at a third the distance of the Sun in both March and December 1 Using the 2021 orbit solution the Earth approach on March 27 2036 will be no closer than 0 3089 AU 46 21 million km 28 71 million mi 120 2 LD but more likely about 0 3097 AU 46 33 million km 28 79 million mi 1 For comparison the planet Venus will be closer to Earth at 0 2883 AU 43 13 million km 26 80 million mi 112 2 LD on May 30 2036 43 c On 31 December 2036 Apophis will be a little bit further away than the March approach at about 0 33 AU 49 million km 31 million mi 2051 approach edit Around April 19 20 2051 Apophis will pass about 0 04 AU 6 0 million km 3 7 million mi from Earth and it will be the first time since 2029 that Apophis will pass within 10 million km of Earth 1 2066 and 2068 edit In the 2060s Apophis will approach Earth in September 2066 1 44 and then from February 2067 to December 2071 Apophis will remain farther from Earth than the Sun is 45 On April 12 2068 JPL Horizons calculates that Apophis will be about 1 864 0 003 AU 278 85 0 45 million km from Earth 46 15 making the asteroid much further than the Sun By 2116 the JPL Small Body Database and NEODyS close approach data start to become divergent 1 44 In April 2116 Apophis is expected to pass about 0 02 AU 3 million km 8 LD from Earth but could pass as close as 0 001 AU 150 thousand km 0 39 LD or could pass as far as 0 1 AU 15 million km 39 LD 1 Refinement of close approach predictions edit Six months after discovery and shortly after a close approach to Earth on December 21 2004 the improved orbital estimates led to the prediction of a very close approach on April 13 2029 by both NASA s automatic Sentry system and NEODyS a similar automatic program run by the University of Pisa and the University of Valladolid Subsequent observations decreased the uncertainty in Apophis s trajectory The probability of an impact event in 2029 temporarily climbed peaking at 2 7 1 in 37 on December 27 2004 47 48 when the uncertainty region had shrunk to 83 000 km 49 This probability combined with its size caused Apophis to be assessed at level 4 on the Torino scale 13 and 1 10 on the Palermo Technical Impact Hazard Scale scales scientists use to represent how dangerous a given asteroid is to Earth These are the highest values for which any object has been rated on either scale The chance that there would be an impact in 2029 was eliminated by late December 27 2004 as a result of a precovery image that extended the observation arc back to March 2004 25 The danger of a 2036 passage was lowered to level 0 on the Torino scale in August 2006 50 With a cumulative Palermo Scale rating of 3 22 3 the risk of impact from Apophis is less than one thousandth the background hazard level 3 2005 and 2011 observations edit In July 2005 former Apollo astronaut Rusty Schweickart as chairman of the B612 Foundation formally asked NASA to investigate the possibility that the asteroid s post 2029 orbit could be in orbital resonance with Earth which would increase the probability of future impacts Schweickart also asked NASA to investigate whether a transponder should be placed on the asteroid to enable more accurate tracking of how its orbit is affected by the Yarkovsky effect 51 On January 31 2011 astronomers took the first new images of Apophis in more than 3 years 52 nbsp Illustration of a common trend where progressively reduced uncertainty regions result in an asteroid impact probability increasing followed by a sharp decrease2013 refinement edit The close approach in 2029 will substantially alter the object s orbit prompting Jon Giorgini of JPL to say in 2011 If we get radar ranging in 2013 the next good opportunity we should be able to predict the location of 2004 MN4 out to at least 2070 53 Apophis passed within 0 0966 AU 14 45 million km 8 98 million mi of Earth in 2013 allowing astronomers to refine the trajectory for future close passes 9 44 54 Just after the closest approach on January 9 2013 44 the asteroid peaked at an apparent magnitude of about 15 6 55 The Goldstone radar observed Apophis during that approach from January 3 through January 17 56 The Arecibo Observatory observed Apophis once it entered Arecibo s declination window after February 13 2013 56 The 2013 observations basically ruled out any chance of a 2036 impact A NASA assessment as of February 21 2013 that did not use the January and February 2013 radar measurements gave an impact probability of 2 3 in a million for 2068 57 As of May 6 2013 using observations through April 15 2013 the odds of an impact on April 12 2068 as calculated by the JPL Sentry risk table had increased slightly to 3 9 in a million 1 in 256 000 3 2015 observations edit As of January 2019 Apophis had not been observed since 2015 mostly because its orbit kept it very near the Sun from the perspective of Earth It was not further than 60 degrees from the Sun between April 2014 and December 2019 With the early 2015 observations the April 12 2068 impact probability was 6 7 in a million 1 in 150 000 and the asteroid had a cumulative 9 in a million 1 in 110 000 chance of impacting Earth before 2106 58 2020 21 observations edit source source source source source source Apophis in February 2021No observations of Apophis were made between January 2015 and February 2019 and then observations started occurring regularly in January 2020 59 In March 2020 astronomers David Tholen and Davide Farnocchia measured the acceleration of Apophis due to the Yarkovsky effect for the first time significantly improving the prediction of its orbit past the 2029 flyby Tholen and Farnocchia found that the Yarkovsky effect caused Apophis to drift by about 170 meters per year 60 In late 2020 Apophis approached the Earth again It passed 0 11265 AU 16 852 million km 43 84 LD from Earth on March 6 2021 brightening to 15 mag at the time Radar observations of Apophis were planned at Goldstone in March 2021 19 The asteroid has been observed by NEOWISE between December 2020 and April 2021 61 62 and by NEOSSat in January 2021 6 63 7 Apophis was the target of an observing campaign by IAWN resulting in the collection of light curves spectra and astrometry 6 63 7 The observations were used to practice and coordinate the response to an actual impact threat 64 nbsp Hypothetical risk corridor for an impact on 13 April 2029 based on the 2020 21 planetary defense exerciseOn February 21 2021 Apophis was removed from the Sentry Risk Table as an impact in the next 100 years was finally ruled out 65 Several occultations of bright stars apparent magnitude 8 11 by Apophis occurred in March and April 2021 66 67 68 69 A total of five separate occultations were observed successfully marking the first time that an asteroid as small as Apophis was observed using the occultation method beating the previous record set in 2019 by asteroid 3200 Phaeton by more than a factor of ten 67 The first event on March 7 was successfully observed from the United States by multiple observers 70 71 66 The next potential occultation which occurred on March 11 was predicted to be visible from central Europe 68 This event was missed mainly because of bad weather two negative observations were recorded from Greece 67 On March 22 another occultation was observed only by a single observer from the United States amateur astronomer Roger Venable Larger than expected residuals in the March 7 data had caused the majority of observers to be deployed outside of the actual path for the March 22 occultation 66 This single detection then allowed the prediction of several more events that would have been unobservable otherwise including an occultation on April 4 which was observed from New Mexico again by Venable alongside others 69 66 Two more occultations observable on April 10 and April 11 from Japan and New Mexico respectively were seen by several observers each 66 On March 9 2021 using radar observations from Goldstone taken on March 3 8 and three positive detections of the stellar occultation on March 7 2021 72 Apophis became the asteroid with the most precisely measured Yarkovsky effect of all asteroids at a signal to noise ratio SNR of 186 4 73 d surpassing 101955 Bennu SNR 181 6 74 The 2021 apparition was the last opportunity to observe Apophis before its 2029 flyby 1 nbsp Asteroid 99942 Apophis radar observations March 8 10 2021 March 26 2021 History of impact estimates edit This section needs additional citations for verification Please help improve this article by adding citations to reliable sources in this section Unsourced material may be challenged and removed July 2008 Learn how and when to remove this template message Date Time Status2004 12 23 The original NASA report mentioned impact chances of around 1 in 300 in 2029 which was widely reported in the media 13 The actual NASA estimates at the time were 1 in 233 these resulted in a Torino scale rating of 2 the first time any asteroid had received a rating above 1 Later that day based on a total of 64 observations the estimates were changed to 1 in 62 1 6 resulting in an update to the initial report and an upgrade to a Torino scale rating of 4 2004 12 25 The chances were first reported as 1 in 42 2 4 and later that day based on 101 observations as 1 in 45 2 2 At the same time the asteroid s estimated diameter was lowered from 440 m to 390 m and its mass from 1 2 1011 kg to 8 3 1010 kg 2004 12 26 Based on a total of 169 observations the impact probability was still estimated as 1 in 45 2 2 the estimates for diameter and mass were lowered to 380 m and 7 5 1010 kg respectively 2004 12 27 Based on a total of 176 observations with an observation arc of 190 days the impact probability was raised to 1 in 37 2 7 48 with a line of variation LOV of only 83 000 km 49 diameter was increased to 390 m and mass to 7 9 1010 kg Later that afternoon a precovery increased the span of observations to 287 days which eliminated the 2029 impact threat 25 The cumulative impact probability was estimated to be around 0 004 a risk lower than that of asteroid 2004 VD17 which once again became the greatest risk object A 2053 approach to Earth still poses a minor risk of impact and Apophis was still rated at level one on the Torino scale for this orbit 2004 12 28 12 23 GMT Based on a total of 139 observations a value of one was given on the Torino scale for 2044 04 13 29 and 2053 04 13 51 2004 12 29 01 10 GMT The only pass rated 1 on the Torino scale was for 2053 04 13 51 based on 139 observations spanning 287 71 days 2004 Mar 15 1104 to 2004 Dec 27 8243 As of February 2013 update the 2053 risk is only 1 in 20 billion 3 19 18 GMT This was still the case based upon 147 observations spanning 288 92 days 2004 Mar 15 1104 to 2004 Dec 29 02821 though the close encounters have changed and been reduced to 4 in total 2004 12 30 13 46 GMT No passes were rated above 0 based upon 157 observations spanning 289 33 days 2004 Mar 15 1104 to 2004 Dec 29 44434 The most dangerous pass was rated at 1 in 7 143 000 22 34 GMT 157 observations spanning 289 33 days 2004 Mar 15 1104 to 2004 Dec 29 44434 One pass at 1 Torino scale 3 other passes 2005 01 02 03 57 GMT Observations spanning 290 97 days 2004 Mar 15 1104 to 2004 Dec 31 07992 One pass at 1 Torino scale 19 other passes 2005 01 03 14 49 GMT Observations spanning 292 72 days 2004 Mar 15 1104 to 2005 Jan 01 82787 One pass at 1 Torino scale 15 other passes 2005 01 Extremely precise radar observations at Arecibo Observatory 26 refine the orbit further and show that the April 2029 close approach will occur at only 5 7 Earth radii 27 approximately one half the distance previously estimated 2005 02 06 Apophis 2004 MN4 had a 1 in 13 000 chance of impacting in April 2036 75 2005 08 07 Radar observation 26 refines the orbit further and eliminates the possibility of an impact in 2035 Only the pass in 2036 remains at Torino scale 1 with a 1 in 5 560 chance of impact 76 2005 10 It is predicted that Apophis will pass just below the altitude of geosynchronous satellites which are at approximately 35 900 kilometres 22 300 mi 77 Such a close approach by an asteroid of that size is estimated to occur every 800 years or so 78 2006 05 06 Radar observation at Arecibo Observatory 26 slightly lowered the Palermo scale rating but the pass in 2036 remained at Torino scale 1 79 despite the impact probability dropping by a factor of four 2006 08 05 Additional observations through 2006 resulted in Apophis being lowered to Torino scale 0 50 The impact probability was 1 in 45 000 50 2008 04 Nico Marquardt published a research paper in which he calculated the probability of Apophis to collide with a geosynchronous satellite during its flyby on April 13 2029 and the consequences of this event to the likelihood of an Earth collision 2036 Afterwards the German newspaper Bild published an article stating a 100 times higher probability of an Earth collision in the year 2036 than Marquardt calculated 80 Nearly all international press reported the news with false data caused by the review from Bild even though Marquardt denied 81 This estimate was allegedly confirmed by ESA and NASA 82 80 but in an official statement 83 NASA denied the wrong statement The release went on to explain that since the angle of Apophis s approach to the Earth s equator means the asteroid will not travel through the belt of current equatorial geosynchronous satellites there is currently no risk of collision and the effect on Apophis s orbit of any such impact would be insignificant 2008 04 16 NASA News Release 08 103 reaffirmed that its estimation of a 1 in 45 000 chance of impact in 2036 remained valid 83 2009 04 29 An animation is released 84 that shows how unmeasured physical parameters of Apophis bias the entire statistical uncertainty region If Apophis is a retrograde rotator on the small less massive end of what is possible the measurement uncertainty region will get pushed back such that the center of the distribution encounters Earth s orbit This would result in an impact probability much higher than computed with the Standard Dynamical Model Conversely if Apophis is a small less massive prograde rotator the uncertainty region is advanced along the orbit Only the remote tails of the probability distribution could encounter Earth producing a negligible impact probability 2009 10 07 Refinements to the precovery images of Apophis by the University of Hawaii s Institute for Astronomy the 90 inch Bok Telescope and the Arecibo Observatory have generated a refined path that reduces the odds of an April 13 2036 impact to about 1 in 250 000 85 Criticism of older published impact probabilities rests on the fact that important physical parameters such as mass and spin that affect its precise trajectory have not yet been accurately measured and hence there are no associated probability distributions The Standard Dynamical Model used for making predictions simplifies calculations by assuming Earth is a point mass this can introduce up to 2 9 Earth radii of prediction error for the 2036 approach and Earth s oblateness must be considered for the 2029 passage to predict a potential impact reliably 78 Additional factors that can greatly influence the predicted motion in ways that depend on unknown details are the spin of the asteroid 86 its precise mass the way it reflects and absorbs sunlight radiates heat and the gravitational pull of other asteroids passing nearby 78 Small uncertainties in the masses and positions of the planets and Sun can cause up to 23 Earth radii of prediction error for Apophis by 2036 78 2013 01 A statistical impact risk analysis of the data up to this point calculated that the odds of the 2036 impact at 7 07 in a billion effectively ruling it out The same study looked at the odds of an impact in 2068 which were calculated at 2 27 in a million 87 First appearance of Sentry virtual impactors that also include mid October dates 88 2013 01 09 The European Space Agency ESA announced the Herschel Space Observatory made new thermal infrared observations of the asteroid as it approached Earth The initial data shows the asteroid to be bigger than first estimated because it is now expected to be less reflective than originally thought 9 The Herschel Space Observatory observations increased the diameter estimate by 20 from 270 to 325 metres which translates into a 75 increase in the estimates of the asteroid s volume or mass 9 Goldstone single pixel observations of Apophis have ruled out the potential 2036 Earth impact 14 89 90 Apophis will then come no closer than about 23 million kilometres 14 10 6 mi and more likely miss us by something closer to 56 million kilometres 35 10 6 mi 89 The radar astrometry is more precise than was expected 89 2016 03 25 The Sentry Risk Table assessed Apophis as having a 6 7 in a million 1 in 150 000 chance of impacting Earth in 2068 and a 9 in a million 1 in 110 000 cumulative chance of impacting Earth by 2105 3 2020 03 By taking observations of Apophis with the Subaru Telescope in January and March 2020 as well as remeasuring older observations using the new Gaia DR2 star catalog astronomers positively detect the Yarkovsky effect on Apophis The asteroid s position is found to shift by 170 meters per year The Yarkovsky effect is the main source of uncertainty in impact probability estimates for this asteroid 60 2021 01 20 The Sentry Risk Table assessed Apophis as having a 2 6 in a million 1 in 380 000 chance of impacting Earth in 2068 and a 4 5 in a million 1 in 220 000 cumulative chance of impacting Earth by 2107 3 The previous 2068 odds were 1 in 150 000 2021 03 15 10 44 JPL solution 207 using observations in 2020 and 2021 reduced the 3 sigma uncertainty region in the 2029 approach distance from 700 km 91 to about 3 km 1 The June 2021 solution showed the Earth approach on March 27 2036 will be no closer than 0 30889 AU 46 209 million km 28 713 million mi 120 21 LD 1 Possible impact effects editThe Sentry Risk Table estimates that Apophis would impact Earth with kinetic energy equivalent to 1 200 megatons of TNT In comparison the Chicxulub impact which caused the mass extinction event responsible for wiping out the dinosaurs has been estimated to have released about as much energy as 100 000 000 megatons 100 teratons The exact effects of any impact would vary based on the asteroid s composition and the location and angle of impact Any impact would be extremely detrimental to an area of thousands of square kilometres but would be unlikely to have long lasting global effects such as the initiation of an impact winter citation needed Assuming Apophis is a 370 metre wide 1 210 ft stony asteroid with a density of 3 000 kg m3 if it were to impact into sedimentary rock Apophis would create a 5 1 kilometre 17 000 ft impact crater 17 3 Expired 2036 path of risk edit In 2008 the B612 Foundation made estimates of Apophis s path if a 2036 Earth impact were to occur as part of an effort to develop viable deflection strategies 92 The result was a narrow corridor a few kilometres wide called the path of risk extending across southern Russia across the north Pacific relatively close to the coastlines of California and Mexico then right between Nicaragua and Costa Rica crossing northern Colombia and Venezuela ending in the Atlantic just before reaching Africa 93 Using the computer simulation tool NEOSim it was estimated that the hypothetical impact of Apophis in countries such as Colombia and Venezuela which were in the path of risk could have more than 10 million casualties 94 A deep water impact in the Atlantic or Pacific oceans would produce an incoherent short range tsunami with a potential destructive radius inundation height of gt 2 m of roughly 1 000 kilometres 620 mi for most of North America Brazil and Africa 3 000 km 1 900 mi for Japan and 4 500 km 2 800 mi for some areas in Hawaii 95 Exploration editOSIRIS APEX post Earth encounter rendezvous edit The OSIRIS REx spacecraft returned a sample of Bennu to Earth on 24 September 2023 96 After ejecting the sample canister the spacecraft can use its remaining fuel to target another body during an extended mission Apophis is the only asteroid which the spacecraft could reach for a long duration rendezvous rather than a brief flyby In April 2022 the extension was approved and OSIRIS REx will perform a rendezvous with Apophis in April 2029 a few days after the close approach to Earth It will study the asteroid for 18 months and perform a maneuver similar to the one it made during sample collection at Bennu by approaching the surface and firing its thrusters This will expose the asteroid s subsurface and allow mission scientists to learn more about the asteroid s material properties 97 98 For its Apophis mission after the sample return OSIRIS REx was renamed OSIRIS APEX short for OSIRIS Apophis Explorer 99 Other proposed space missions edit Planetary Society competition edit This section needs additional citations for verification Please help improve this article by adding citations to reliable sources in this section Unsourced material may be challenged and removed December 2020 Learn how and when to remove this template message In 2007 The Planetary Society a California based space advocacy group organized a 50 000 competition to design an uncrewed space probe that would shadow Apophis for almost a year taking measurements that would determine whether it will impact Earth thus helping governments decide whether to mount a deflection mission to alter its orbit The society received 37 entries from 20 countries on 6 continents The commercial competition was won by a design called Foresight created by SpaceWorks Enterprises Inc 100 SpaceWorks proposed a simple orbiter with only two instruments and a radio beacon at a cost of US 140 million launched aboard a Minotaur IV between 2012 and 2014 to arrive at Apophis five to ten months later It would then rendezvous with observe and track the asteroid Foresight would orbit the asteroid to gather data with a multi spectral imager for one month It would then leave orbit and fly in formation with Apophis around the Sun at a range of two kilometres 1 2 miles The spacecraft would use laser ranging to the asteroid and radio tracking from Earth for ten months to accurately determine the asteroid s orbit and how it might change Pharos the winning student entry would be an orbiter with four science instruments a multi spectral imager near infrared spectrometer laser rangefinder and magnetometer that would rendezvous with and track Apophis Earth based tracking of the spacecraft would then allow precise tracking of the asteroid The Pharos spacecraft would also carry four instrumented probes that it would launch individually over the course of two weeks Accelerometers and temperature sensors on the probes would measure the seismic effects of successive probe impacts a creative way to explore the interior structure and dynamics of the asteroid Second place for 10 000 went to a European team led by Deimos Space S L of Madrid Spain in cooperation with EADS Astrium Friedrichshafen Germany University of Stuttgart Germany and University of Pisa Italy Juan L Cano was principal investigator Another European team took home 5 000 for third place Their team lead was EADS Astrium Ltd United Kingdom in conjunction with EADS Astrium SAS France IASF Roma INAF Rome Italy Open University UK Rheinisches Institut fur Umweltforschung Germany Royal Observatory of Belgium and Telespazio Italy The principal investigator was Paolo D Arrigo Two teams tied for second place in the Student Category Monash University Clayton Campus Australia with Dilani Kahawala as principal investigator and University of Michigan with Jeremy Hollander as principal investigator Each second place team won 2 000 A team from Hong Kong Polytechnic University and Hong Kong University of Science and Technology under the leadership of Peter Weiss received an honorable mention and 1 000 for the most innovative student proposal Don Quijote mission edit Apophis is one of two asteroids that were considered by the European Space Agency as the target of its Don Quijote mission concept to study the effects of impacting an asteroid 101 Cancelled Chinese mission edit China had planned an encounter with Apophis in 2022 several years prior to the close approach in 2029 This mission now known as Tianwen 2 would have included exploration and close study of three asteroids including an extended encounter with Apophis for close observation and land on the asteroid 1996 FG3 to conduct in situ sampling analysis on the surface 102 The launch date is now scheduled for 2024 with a different set of targets RAMSES edit Apophis is the target of the European Space Agency s proposed RAMSES Rapid Apophis Mission for SEcurity and Safety mission with a launch in 2027 and rendezvous with the asteroid in 2029 103 Proposed deflection strategies editFurther information Asteroid impact avoidance Studies by NASA ESA 104 and various research groups in addition to the Planetary Society contest teams 105 have described a number of proposals for deflecting Apophis or similar objects including gravitational tractor kinetic impact and nuclear bomb methods On December 30 2009 Anatoly Perminov the director of the Russian Federal Space Agency said in an interview that Roscosmos will also study designs for a possible deflection mission to Apophis 106 On August 16 2011 researchers at China s Tsinghua University proposed launching a mission to knock Apophis onto a safer course using an impactor spacecraft in a retrograde orbit steered and powered by a solar sail Instead of moving the asteroid on its potential resonant return to Earth Shengping Gong and his team believe the secret is shifting the asteroid away from entering the gravitational keyhole in the first place 107 On February 15 2016 Sabit Saitgarayev of the Makeyev Rocket Design Bureau announced intentions to use Russian ICBMs to target relatively small near Earth objects Although the report stated that likely targets would be between the 20 to 50 metres in size it was also stated that 99942 Apophis would be an object subject to tests by the program 108 In October 2022 a method of mapping the inside of a potentially problematic asteroid such as 99942 Apophis in order to determine the best area for impact was proposed 109 Popular culture editIn Id Software s video game Rage the backstory involves the asteroid colliding with Earth on August 23 2029 The asteroid almost wipes out the human race and ushers in a post apocalyptic age 110 See also editAsteroid capture Asteroid impact prediction Asteroid Redirect Mission Earth grazing fireball List of impact craters on Earth NEO SurveyorNotes edit Of the six asteroids with a riskier palermo scale rating than Apophis 29075 1950 DA and 101955 Bennu can not impact within the next 100 years 1979 XB and 2007 FT3 are lost short arc objects that can not be recovered with targeted observations and await serendipitous survey observations 2000 SG344 and 2009 JF1 are less than 50 meters in diameter The minimum possible Earth approach between 5 20 April 2116 is 0 001 AU 150 thousand km 93 thousand mi 0 39 LD On January 8 2022 Venus was even closer to Earth at 0 2658 AU 39 76 million km 24 71 million mi 103 4 LD Using the 9 March 2021 solution JPL gave the strength of the Yarkovsky effect as A 2 2 877 10 14 AU d 2 displaystyle A 2 2 877 times 10 14 text AU d 2 nbsp with an uncertainty of 1 543 10 16 AU d 2 displaystyle 1 543 times 10 16 text AU d 2 nbsp The SNR defined as the size of the signal divided by the uncertainty is 2 877 10 14 1 543 10 16 186 4 displaystyle 2 877 times 10 14 1 543 times 10 16 186 4 nbsp As of the latest orbit solution 29 June 2021 the SNR is 2 901 10 14 1 942 10 16 149 4 displaystyle 2 901 times 10 14 1 942 times 10 16 149 4 nbsp again lower than Bennu s References edit a b c d e f g h i j k l m n o p q r s t u JPL Small Body Database Browser 99942 Apophis 2004 MN4 last observation 2021 05 12 arc 17 16 years JPL 216 solution date 2021 Jun 29 Retrieved November 27 2021 a b c d e f Brozovic M Benner L A M McMichael J G Giorgini J D et al January 15 2018 Goldstone and Arecibo radar observations of 99942 Apophis in 2012 2013 PDF Icarus 300 115 128 Bibcode 2018Icar 300 115B doi 10 1016 j icarus 2017 08 032 Retrieved August 19 2018 a b c d e f g h i j k l m 99942 Apophis 2004 MN4 Earth Impact Risk Summary NASA JPL Center for NEO Studies January 19 2021 Archived from the original on May 11 2013 Retrieved January 19 2021 Binzel R P 2007 Can NEAs be Grouped by Their Common Physical Characteristics PDF Department of Earth Atmospheric and Planetary Sciences Massachusetts Institute of Technology aero org Archived from the original PDF on April 12 2012 a b c 99942 Apophis The Near Earth Asteroids Data Base at E A R N Archived from the original on June 16 2012 Retrieved October 15 2009 a b c Reddy Vishnu Kelley Michael S Dotson Jessie Farnocchia Davide et al May 31 2022 Apophis Planetary Defense Campaign The Planetary Science Journal 3 5 123 Bibcode 2022PSJ 3 123R doi 10 3847 PSJ ac66eb S2CID 249227833 a b c 99942 Apophis 2021 Gallery IAWN March 19 2021 Retrieved June 1 2022 a b c d Pravec P Scheirich P Durech J Pollock J et al 2014 The tumbling spin state of 99942 Apophis PDF Icarus 233 48 60 Bibcode 2014Icar 233 48P doi 10 1016 j icarus 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Gamespot External links edit nbsp Wikimedia Commons has media related to 99942 Apophis Muller T G Kiss C Scheirich P Pravec P et al 2014 Thermal infrared observations of asteroid 99942 Apophis with Herschel Astronomy amp Astrophysics 566 A22 arXiv 1404 5847 Bibcode 2014A amp A 566A 22M doi 10 1051 0004 6361 201423841 S2CID 119282830 Apophis Asteroid Asteroid Apophis orbit from recent observations EPSC Abstracts Vol 6 EPSC DPS2011 1212 2011 EPSC DPS Joint Meeting 2011 Diagrams and orbits of Apophis Sormano Astronomical Observatory Interactive 3D gravity simulation of Apophis s 2029 Earth flybyRisk assessment Apophis Orbital Prediction Page at NASA JPL 99942 Apophis page from NEODyS MBPL Minor Body Priority List technical List at Sormano Observatory TECA Table of Asteroids Next Closest Approaches to the Earth at Sormano ObservatoryNASA Possibility of an Earth Impact in 2029 Ruled Out for Asteroid 2004 MN4 JPL Radar Observations Refine the Future Motion of Asteroid 2004 MN4 JPL Animation explaining how impact risk is determined from Impact Probability 99942 Apophis at the JPL Small Body DatabaseClose approach Discovery Ephemeris Orbit diagram Orbital elements Physical parametersPreceded by 153814 2001 WN5 Large NEO Earth close approach inside the orbit of the Moon 13 April 2029 Succeeded by2012 UE34 Portals nbsp Physics nbsp Astronomy nbsp Stars nbsp Spaceflight nbsp Outer space nbsp Solar System nbsp Science Retrieved from https en wikipedia org w index php title 99942 Apophis amp oldid 1209446199, wikipedia, wiki, book, books, library,

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