EOS-AM 1 |
USA |
Spacecraft n°: |
USA satellite n°: |
Launch data:
|
Prime contractor | Lockheed Martin |
Platform | |
Mass at launch | 4854 kg |
Mass in orbit | |
Paylaod mass | 1100 kg |
Dimension | |
Solar array | |
Stabilization | 3-axis |
DC power | 7500 W |
Design lifetime | 6 years |
Ref.: #15 - update: 16.03.09 | Home |