Specifications
|
Prime
contractor
|
GE
Astro
|
|
Platform
|
MultiMission
Spacecraft bus
|
|
Mass
at launch
|
6800
kg (2500 kg for the payload)
|
|
Diameter
|
5
m
|
|
Height
|
10
m
|
|
Solar
array
|
1.5
x 3.3 m
|
|
Stabilization
|
3
axis
|
|
Design
lifetime
|
3
years
|
|
End of live:
| Reentered date: | 24 Sep 2011 - 04:00 UT |
| Lifetime: | |
|