Spacecraft data:
| Prime manufacturer | ISRO |
| Platform | I-2K (I-2000) bus |
| Operator | Insat |
| Mass at launch | 2117 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | 5 C × S transponders (9 MHz bandwidth), 5 S × C transponders (2.7 MHz bandwidth) |
| Solar array | |
| Stabilization | |
| Propulsion | 440 Newton thrust liquid apogee motor |
| DC power | 2 deployable solar arrays |
| Design lifetime | 9 yrs |
|
Location:
| Date | Position | Remarks |
| Sep 2015 | 83° E | |
|