Names | Navstar 2A-03 GPS IIA-3 GPS II-12 GPS SVN-25 |
---|---|
Mission type | Navigation |
Operator | U.S. Air Force |
COSPAR ID | 1992-009A [1] |
SATCAT no. | 21890 |
Mission duration | 7.5 years (planned) 17.75 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 | 23 February 1992, 22:29:00 UTC |
Rocket | Delta II 7925-9.5 (Delta D207) |
Launch site | Cape Canaveral, LC-17B |
Contractor | McDonnell Douglas |
Entered service | 27 March 1992 |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | 18 December 2009 |
Orbital parameters | |
Reference system | Geocentric orbit[3] |
Regime | Medium Earth orbit (Semi-synchronous) |
Slot | A2 (slot 2 plane A) |
Perigee altitude | 19,913 km (12,373 mi) |
Apogee altitude | 20,318 km (12,625 mi) |
Inclination | 54.70° |
Period | 714.70 minutes |
USA-79, also known as GPS IIA-3, GPS II-12 and GPS SVN-25, was an American navigation satellite which formed part of the Global Positioning System. It was the third of nineteen Block IIA GPS satellites to be launched.