Jump to content

USA-168

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by WDGraham (talk | contribs) at 01:25, 16 December 2013 (recategorise, genfixes, replaced: Category:2003 in spaceflightCategory:Spacecraft launched in 2003 using AWB). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

USA-168
A Block IIR GPS satellite
Mission typeNavigation
OperatorUS Air Force
COSPAR ID2003-010A[1]
SATCAT no.27704[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 date31 March 2003, 22:09:01 (2003-03-31UTC22:09:01Z) UTC
RocketDelta II 7925-9.5, D297[3]
Launch siteCape Canaveral SLC-17A[3]
Orbital parameters
Reference systemGeocentric
RegimeMedium Earth
(Semi-synchronous)
Perigee altitude20,063 kilometres (12,467 mi)[4]
Apogee altitude20,433 kilometres (12,696 mi)[4]
Inclination54.9 degrees[4]
Period720.64 minutes[4]

USA-168, also known as GPS IIR-9 and GPS SVN-45, is an American navigation satellite which forms part of the Global Positioning System. It was the ninth 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-168 was launched at 22:09:01 UTC on 31 March 2003, atop a Delta II carrier rocket, flight number D297, 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-168 into a transfer orbit. The satellite raised itself into medium Earth orbit using a Star-37FM apogee motor.[2]

By 3 April 2003, USA-168 was in an orbit with a perigee of 20,063 kilometres (12,467 mi), an apogee of 20,433 kilometres (12,696 mi), a period of 720.64 minutes, and 54.9 degrees of inclination to the equator.[4] It is used to broadcast the PRN 21 signal, and operates in slot 3 of plane D of the GPS constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years.[2] As of 2012 it remains in service.

References

  1. ^ a b "Navstar 52". 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.