|
| GPS
2A-20
|
|
Satellite
|
| Int'l Designation |
1993
032A
|
Active
|
| Owner / Sponsor |
USAF
|
| Mission |
Navigation
|
| Constellation /
Block |
NAVSTAR
GPS / Block
IIA
|
| Launch Mass |
1816
kg (4002 lbm)
|
| Dimensions, stowed |
|
| Mission Orbit |
MEO /
20,200 km (10, 900 nmi)
|
55°
|
| Transponders |
2
L-band
1 S-band
|
| Design Life |
7.5
years
|
| Power (EOL) |
0.710
kW
|
| Other names |
SVN
37
|
| Service History |
Unusable
1999 Apr 20 0437 UTC to 1999 Apr 26 1533 UTC due to change
in operational frequency standard from Cs to Rb
Unusable 1994 Mar 30 0730 UTC to 1994 Apr 04 1330 UTC due to
change in operational Cs frequency standards
|
|
Launch
|
| Launch Vehicle
Model |
Delta
II 7925 |
| Date / Time (UTC) |
1993
May 13
|
00:07
|
|
Financial
|
| Satellite cost |
|
| Web Links |
|
|
|
