Names | Navstar 2A-08 GPS IIA-8 GPS II-17 GPS SVN-29 |
---|---|
Mission type | Navigation |
Operator | U.S. Air Force |
COSPAR ID | 1992-089A [1] |
SATCAT no. | 22275 |
Mission duration | 7.5 years (planned) 14.75 years (achieved) |
Spacecraft properties | |
Spacecraft | GPS IIA |
Spacecraft type | GPS Block IIA[2] |
Manufacturer | Rockwell International |
Launch mass | 840 kg (1,850 lb) |
Dimensions | 5.3 m (17 ft) of long |
Power | 710 watts |
Start of mission | |
Launch date | 18 December 1992, 22:16:00 UTC |
Rocket | Delta II 7925-9.5 (Delta D217) |
Launch site | Cape Canaveral, LC-17B |
Contractor | McDonnell Douglas |
Entered service | 25 January 1993 |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | 23 October 2007 |
Orbital parameters | |
Reference system | Geocentric orbit[3] |
Regime | Medium Earth orbit (Semi-synchronous) |
Slot | F5 (slot 5 plane F) |
Perigee altitude | 20,137 km (12,513 mi) |
Apogee altitude | 20,541 km (12,764 mi) |
Inclination | 54.74° |
Period | 720.00 minutes |
USA-87, also known as GPS IIA-8, GPS II-17 and GPS SVN-29, was an American navigation satellite which formed part of the Global Positioning System. It was the eighth of nineteen Block IIA GPS satellites to be launched.