Specifications
| Prime contractor | Lockheed Martin Missiles and Space |
| Platform | |
| Operator | US Air Force |
|
Mass
at launch | 1156 kg |
|
Dry
mass | 884 kg |
|
Dimension
|
|
|
Solar
array
|
|
|
Stabilization
|
3-axis
|
|
DC
power
|
BOL:
1700 W
EOL: 1230 W
|
|
Design
lifetime
| 10 yrs - still active |
|
Location:
| Date | Position | Remarks |
| April 2010 | 60.01° E | |
|