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USA-266

USA-266, also known as GPS IIF-12, GPS SVN-70 and NAVSTAR 76, is an American navigation satellite which forms part of the Global Positioning System. It was the twelfth of twelve Block IIF satellites to be launched.[2]

USA-266
A Block IIF GPS satellite
NamesGPS IIF-12
GPS SVN-70
NAVSTAR 76
Mission typeNavigation
OperatorUS Air Force
COSPAR ID2016-007A [1]
SATCAT no.41328
Mission duration12 years (planned)
Spacecraft properties
SpacecraftGPS SVN-70 (IIF-12)
Spacecraft typeGPS Block IIF
ManufacturerBoeing
Launch mass1,630 kg (3,590 lb) [2]
Start of mission
Launch date5 February 2016, 13:38 UTC
RocketAtlas V 401 (AV-057) [3]
Launch siteCCAFS, SLC-41
ContractorULA
Entered service9 March 2016
Orbital parameters
Reference systemGeocentric orbit
RegimeMedium Earth orbit
(Semi-synchronous)
Perigee altitude20,196 km (12,549 mi)
Apogee altitude20,181 km (12,540 mi)
Inclination55.01°
Period717.9 minutes
 

Launch edit

Built by Boeing and launched by United Launch Alliance (ULA), USA-266 was launched at 13:38 UTC on 5 February 2016, atop an Atlas V 401 launch vehicle, vehicle number AV-057.[3] The launch took place from Space Launch Complex 41 at the Cape Canaveral Air Force Station,[4] and placed USA-266 directly into semi-synchronous orbit.[5]

Orbit edit

As of March 2016, USA-266 was in an orbit with a perigee of 20,181 km (12,540 mi), an apogee of 20,196 km (12,549 mi), a period of 717.9 minutes, and 55.01° of inclination to the equator.[5] It is used to broadcast the PRN 32 signal, and operates in slot 5 of plane F of the GPS constellation.[6] The satellite has a design life of 12 years and a mass of 1,630 kg (3,590 lb).[2] It is currently in service following commissioning on 9 March 2016.[7]

References edit

  1. ^ "Navstar 76". NASA. Retrieved 13 March 2016.   This article incorporates text from this source, which is in the public domain.
  2. ^ a b c Krebs, Gunter. "GPS-2F (Navstar-2F)". Gunter's Space Page. Retrieved 13 March 2016.
  3. ^ a b McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 13 March 2016.
  4. ^ McDowell, Jonathan. "Launch List". Launch Vehicle Database. Jonathan's Space Page. Retrieved 13 March 2016.
  5. ^ a b McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 13 March 2016.
  6. ^ "GPS Constellation Status". US Department of Homeland Security. Retrieved 8 April 2016.   This article incorporates text from this source, which is in the public domain.
  7. ^ "NOTICE ADVISORY TO NAVSTAR USERS (NANU) 2016022". United States Coast Guard. Retrieved 13 March 2016.


also, known, navstar, american, navigation, satellite, which, forms, part, global, positioning, system, twelfth, twelve, block, satellites, launched, block, satellitenamesgps, 12gps, 70navstar, 76mission, typenavigationoperatorus, forcecospar, id2016, 007a, sa. USA 266 also known as GPS IIF 12 GPS SVN 70 and NAVSTAR 76 is an American navigation satellite which forms part of the Global Positioning System It was the twelfth of twelve Block IIF satellites to be launched 2 USA 266A Block IIF GPS satelliteNamesGPS IIF 12GPS SVN 70NAVSTAR 76Mission typeNavigationOperatorUS Air ForceCOSPAR ID2016 007A 1 SATCAT no 41328Mission duration12 years planned Spacecraft propertiesSpacecraftGPS SVN 70 IIF 12 Spacecraft typeGPS Block IIFManufacturerBoeingLaunch mass1 630 kg 3 590 lb 2 Start of missionLaunch date5 February 2016 13 38 UTCRocketAtlas V 401 AV 057 3 Launch siteCCAFS SLC 41ContractorULAEntered service9 March 2016Orbital parametersReference systemGeocentric orbitRegimeMedium Earth orbit Semi synchronous Perigee altitude20 196 km 12 549 mi Apogee altitude20 181 km 12 540 mi Inclination55 01 Period717 9 minutes Launch editBuilt by Boeing and launched by United Launch Alliance ULA USA 266 was launched at 13 38 UTC on 5 February 2016 atop an Atlas V 401 launch vehicle vehicle number AV 057 3 The launch took place from Space Launch Complex 41 at the Cape Canaveral Air Force Station 4 and placed USA 266 directly into semi synchronous orbit 5 Orbit editAs of March 2016 USA 266 was in an orbit with a perigee of 20 181 km 12 540 mi an apogee of 20 196 km 12 549 mi a period of 717 9 minutes and 55 01 of inclination to the equator 5 It is used to broadcast the PRN 32 signal and operates in slot 5 of plane F of the GPS constellation 6 The satellite has a design life of 12 years and a mass of 1 630 kg 3 590 lb 2 It is currently in service following commissioning on 9 March 2016 7 References edit nbsp Spaceflight portal Navstar 76 NASA Retrieved 13 March 2016 nbsp This article incorporates text from this source which is in the public domain a b c Krebs Gunter GPS 2F Navstar 2F Gunter s Space Page Retrieved 13 March 2016 a b McDowell Jonathan Launch Log Jonathan s Space Page Retrieved 13 March 2016 McDowell Jonathan Launch List Launch Vehicle Database Jonathan s Space Page Retrieved 13 March 2016 a b McDowell Jonathan Satellite Catalog Jonathan s Space Page Retrieved 13 March 2016 GPS Constellation Status US Department of Homeland Security Retrieved 8 April 2016 nbsp This article incorporates text from this source which is in the public domain NOTICE ADVISORY TO NAVSTAR USERS NANU 2016022 United States Coast Guard Retrieved 13 March 2016 nbsp This article about one or more spacecraft of the United States is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title USA 266 amp oldid 1192219715, wikipedia, wiki, book, books, library,

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