Specifications
| Prime contractor | University of California, Berkeley
|
| Platform | |
| Operator | Mission and Science Operations Center, UC Berkeley/NASA
|
|
Mass
at launch
|
191
kg
|
|
Payload
mass
|
51
kg
|
|
Dimension
|
octogonal
|
|
Solar
array
|
|
|
Stabilization
|
spin
stabilized, 12 rpm
|
|
DC
power | 52 W |
|
Design
lifetime
| 1 yr - still active |
|
|