Spacecraft data:
| Prime manufacturer | |
| Platform | |
| Operator | |
| Mass at launch | 975 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | Three solid state Push Broom Cameras:
- LISS-1(72.5 metre resolution),
- LISS-2A and
- LISS-2B (36.25 metre resolution)
|
| Solar array | |
| Communication | S-band, X-band and VHF(commanding only) |
| Stabilization | Three axis body stabilized (zero momentum)
with 4 Reactions Wheels, Magnetic torquers |
| RCS | Monopropellant Hydrazine based with sixteen 1 Newton thrusters |
| DC power | 600 W |
| Design lifetime | |
|
End of live:
| End of Operation: | July 1996 |
| Cause: | |
|