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 |
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Location:
Date | Position | Remarks |
Sep 2015 | 83° E | |
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