Name:INSAT-2D
LaunchDate:04.06.1997
Become Inoperable in October 1997 due to power bus anomaly.
Replaced by INSAT-2DT.
Replaced by INSAT-2DT.
| Mission | Communication |
| Weight | 2079 kg with propellants, 995 kg dry weight |
| onboard power | 1650 Watts |
| Communication | C,extended C, S and Ku bands |
| Stabilization | Three axis stabilized with two Momen'tum Wheels & one Reaction Wheel,Magnetic torquers |
| Propulsion | Integrated bipropellan stystem ( MMH and N24) With sixteen 22N thrusters and 440N LAM. 0 |
| Payload | Transponders: 16C-band / extended C-band transponders (forFSS), 2 high power C-band transponders (for BSS), 1S-band transponder (for BSS),1C/S-band mobile communication transponder, 3 Ku-band transponders |
| Launch date | June 4, 1997 |
| Launch site | French Guyana |
| Launch vehicle | Arianev 4 |
| Orbit | Geostationary 93,.5deg.E |
| Inclination | 0 deg. |
| Mission life | Seven years(nominal) |
| Orbit life | Very Long |
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