Names | Navstar 2A-02 GPS IIA-2 GPS II-11 GPS SVN-24 |
---|---|
Mission type | Navigation |
Operator | U.S. Air Force |
COSPAR ID | 1991-047A [1] |
SATCAT no. | 21552 |
Mission duration | 7.5 years (planned) 20 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 | 4 July 1991, 02:32:00 UTC |
Rocket | Delta II 7925-9.5 (Delta D206) [3] |
Launch site | Cape Canaveral, LC-17A |
Contractor | McDonnell Douglas |
Entered service | 14 August 1991 |
End of mission | |
Disposal | Graveyard orbit |
Deactivated | 30 September 2011 |
Orbital parameters | |
Reference system | Geocentric orbit[4] |
Regime | Medium Earth orbit (Semi-synchronous) |
Slot | D1 (slot 1 plane D) |
Perigee altitude | 19,451 km (12,086 mi) |
Apogee altitude | 20,250 km (12,580 mi) |
Inclination | 55.30° |
Period | 704.60 minutes |
USA-71, also known as GPS IIA-2, GPS II-11 and GPS SVN-24, is an American navigation satellite which forms part of the Global Positioning System. It was the second of nineteen Block IIA GPS satellites to be launched.
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