Specifications:
| Prime contractor | Ball Aerospace, USA |
| Platform | BCP-2000 |
| Operator | Earth Science Data and Information System (NASA) |
|
Mass
at launch
| 959 kg (1270 kg?) |
| Dry Mass, | 882 kg (970 kg?) |
| Payload
mass |
298
kg |
| Dimension | |
| Solar array | |
| Stabilization | 3-axis |
|
DC
power
|
730
W
|
|
Design
lifetime
|
5
years
|
|
 Illustration of ICESat being integrated at VAFB, CA (image credit: NASA, Boeing) |