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USA-154

USA-154, also known as GPS IIR-6 and GPS SVN-41, is an American navigation satellite which forms part of the Global Positioning System. It was the sixth Block IIR GPS satellite to be launched, out of thirteen in the original configuration, and twenty one overall. It was built by Lockheed Martin, using the AS-4000 satellite bus.[2]

USA-154
A Block IIR GPS satellite
Mission typeNavigation
OperatorUS Air Force
COSPAR ID2000-071A[1]
SATCAT no.26605[1]
Mission duration10 years (planned)[2]
Spacecraft properties
Spacecraft typeGPS Block IIR[2]
BusAS-4000[2]
ManufacturerLockheed Martin[2]
Launch mass2,032 kilograms (4,480 lb)[2]
Start of mission
Launch date10 November 2000, 17:14:02 (2000-11-10UTC17:14:02Z) UTC
RocketDelta II 7925-9.5, D281[3]
Launch siteCape Canaveral SLC-17A[3]
End of mission
Deactivated09 July 2020 (2020-07-10)
Orbital parameters
Reference systemGeocentric
RegimeMedium Earth
(Semi-synchronous)
Perigee altitude20,177 kilometres (12,537 mi)[4]
Apogee altitude20,498 kilometres (12,737 mi)[4]
Inclination55 degrees[4]
Period724.28 minutes[4]
 

USA-154 was launched at 17:14:02 UTC on 10 November 2000, atop a Delta II carrier rocket, flight number D281, flying in the 7925-9.5 configuration.[3] The launch took place from Space Launch Complex 17A at the Cape Canaveral Air Force Station,[5] and placed USA-154 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-37FM apogee motor.[2]

By 13 November 2000, USA-154 was in an orbit with a perigee of 20,177 kilometres (12,537 mi), an apogee of 20,498 kilometres (12,737 mi), a period of 724.28 minutes, and 55 degrees of inclination to the equator.[4] It was used to broadcast the PRN 14 signal, and operated in slot 5 of plane F of the GPS constellation.[6] The satellite had a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years.[2] As of July 2020 it is no longer in service.

References

  1. ^ a b "Navstar 49". US National Space Science Data Center. Retrieved 11 July 2012.
  2. ^ a b c d e f g h Krebs, Gunter. "GPS-2R (Navstar-2R)". Gunter's Space Page. Retrieved 11 July 2012.
  3. ^ a b c McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 11 July 2012.
  4. ^ a b c d e McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 11 July 2012.
  5. ^ McDowell, Jonathan. "Launch List". Launch Vehicle Database. Jonathan's Space Page. Retrieved 11 July 2012.
  6. ^ "GPS Constellation Status". Retrieved 17 July 2020.


also, known, american, navigation, satellite, which, forms, part, global, positioning, system, sixth, block, satellite, launched, thirteen, original, configuration, twenty, overall, built, lockheed, martin, using, 4000, satellite, block, satellitemission, type. USA 154 also known as GPS IIR 6 and GPS SVN 41 is an American navigation satellite which forms part of the Global Positioning System It was the sixth Block IIR GPS satellite to be launched out of thirteen in the original configuration and twenty one overall It was built by Lockheed Martin using the AS 4000 satellite bus 2 USA 154A Block IIR GPS satelliteMission typeNavigationOperatorUS Air ForceCOSPAR ID2000 071A 1 SATCAT no 26605 1 Mission duration10 years planned 2 Spacecraft propertiesSpacecraft typeGPS Block IIR 2 BusAS 4000 2 ManufacturerLockheed Martin 2 Launch mass2 032 kilograms 4 480 lb 2 Start of missionLaunch date10 November 2000 17 14 02 2000 11 10UTC17 14 02Z UTCRocketDelta II 7925 9 5 D281 3 Launch siteCape Canaveral SLC 17A 3 End of missionDeactivated09 July 2020 2020 07 10 Orbital parametersReference systemGeocentricRegimeMedium Earth Semi synchronous Perigee altitude20 177 kilometres 12 537 mi 4 Apogee altitude20 498 kilometres 12 737 mi 4 Inclination55 degrees 4 Period724 28 minutes 4 USA 154 was launched at 17 14 02 UTC on 10 November 2000 atop a Delta II carrier rocket flight number D281 flying in the 7925 9 5 configuration 3 The launch took place from Space Launch Complex 17A at the Cape Canaveral Air Force Station 5 and placed USA 154 into a transfer orbit The satellite raised itself into medium Earth orbit using a Star 37FM apogee motor 2 By 13 November 2000 USA 154 was in an orbit with a perigee of 20 177 kilometres 12 537 mi an apogee of 20 498 kilometres 12 737 mi a period of 724 28 minutes and 55 degrees of inclination to the equator 4 It was used to broadcast the PRN 14 signal and operated in slot 5 of plane F of the GPS constellation 6 The satellite had a mass of 2 032 kilograms 4 480 lb and a design life of 10 years 2 As of July 2020 it is no longer in service References Edit a b Navstar 49 US National Space Science Data Center Retrieved 11 July 2012 a b c d e f g h Krebs Gunter GPS 2R Navstar 2R Gunter s Space Page Retrieved 11 July 2012 a b c McDowell Jonathan Launch Log Jonathan s Space Page Retrieved 11 July 2012 a b c d e McDowell Jonathan Satellite Catalog Jonathan s Space Page Retrieved 11 July 2012 McDowell Jonathan Launch List Launch Vehicle Database Jonathan s Space Page Retrieved 11 July 2012 GPS Constellation Status Retrieved 17 July 2020 Spaceflight portal 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 154 amp oldid 1064468601, wikipedia, wiki, book, books, library,

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