Names | GPS I-7 GPS SVN-7 |
---|---|
Mission type | Navigation Technology |
Operator | U.S. Air Force |
Mission duration | 5 years (planned) Launch failure |
Spacecraft properties | |
Spacecraft | Navstar |
Spacecraft type | GPS Block I |
Manufacturer | Rockwell Space Systems[1] |
Launch mass | 758 kg (1,671 lb) [1] |
Dimensions | 5.3 meters of long |
Power | 400 watts |
Start of mission | |
Launch date | 19 December 1981, 01:10:00 UTC |
Rocket | Atlas E / SGS-1 (Atlas-76E) [2] |
Launch site | Vandenberg, SLC-3E |
Contractor | Convair General Dynamics |
Entered service | Launch failure |
Orbital parameters | |
Reference system | Geocentric orbit (planned) |
Regime | Medium Earth orbit (Semi-synchronous) |
Altitude | 20,200 km |
Inclination | 63.0° |
Period | 720 minutes |
Navstar 7, also known as GPS I-7 and GPS SVN-7, was an American navigation satellite which was lost in a launch failure in 1981. It was intended to be used in the Global Positioning System development program. It was the seventh of eleven Block I GPS satellites to be launched, and the only one to fail to achieve orbit.[1]