|
The mission orbit of the US$44 million 2032 kg (4479 lbm) satellite
will be a
12-hour, 20,200 km (10,900 nmi) altitude orbit, inclined at 55°. This
was the
sixth Block 2R satellite, of a block order of 21, to be supplied
by Lockheed Martin. The satellite design is based on Lockheed
Martin’s AS-4000 series satellite bus, having a design life of 10
years. This launch inserted the satellite into
the F-1 slot of the constellation. While the GPS 2R-6 satellite
did not replace a specific satellite in the existing constellation the
spacecraft which was in the F-1 position, GPS 2A-17, was shifted to slot F-5 for the remainder of its operational life.
| GPS
2R-6 (41)
|
|
Satellite
|
| Int'l Designation |
2000
071A
|
launched
|
| Owner / Sponsor |
USAF
|
| Mission |
Navigation
|
| Constellation/Block |
NAVSTAR
GPS / Block IIR
|
| Launch Mass |
2032
kg (4478 lbm)
|
| Dimensions, stowed |
152
x 193 x 191 cm (5 x 6.33 x 6.25 ft)
|
| Mission Orbit |
MEO /
20,200 km (10,900 nmi)
|
55°
|
| Transponders |
2
L-band, 1 S-band
|
| Design Life |
10
years
|
| Power (EOL) |
1.136
kW
|
| Other names |
SVN
41
|
|
Launch
|
| Launch Vehicle
Model |
Delta
II 7925-9.5 |
| Date / Time (UTC) |
2000
Nov 10
|
17:14
|
|
Financial
|
| Satellite cost |
US$44 million
|
| Web Links |
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