Specifications:
| Prime contractor | Surrey Satellite Technology Ltd. (SSTL) |
| Platform | Microsat-100 |
| Operator | National Space Research and Development Agency (NASRDA) |
| Mass at launch | 98 kg |
| Mass in orbit | 95 kg |
| Dimension | 0.6 x 0.6 x 0.6 m |
| Solar array | Solar cells, batteries |
| Stabilization | 6m gravity gradient boom + momentum wheel |
| Equipment | 32-meter resolution imager in 3 spectral bands |
| Propulsion | |
| DC power | 240 W |
| Design lifetime | 5 yrs |
|
End of live:
| Out of service: | July 2012 |
| Cause: | |
|