Spacecraft data:
| Prime contractor | ISRO |
| Operator | Indian Space Research Organization (ISRO) |
| Platform | |
| Mass at launch | 3025 kg |
| Dry Mass | 1335 kg |
| Basic shape | Box+ 2panels + 2dishes |
| Dimension (m) | 2.0x1.77x3.10
15.4 span |
| Solar array | |
| Stabilization | It uses 3 earth sensors, 2 digital sun sensors, 8 coarse analog sun sensors, 3 solar
panel sun sensors and one sensor processing electronics. The wheels and wheel drive electronics were imported with indigenous wheel interface module to interface the wheel drive electronics and AOCE. |
| Propulsion | The propulsion system is employing 16 thrusters, 4 each located on east, west and AY
sides and 2 each on north and south sides. There is one 440 N liquid apogee motor (using Mono Methyl Hydrazine (MMH) as
fuel and oxides of Nitrogen ( MON3 as oxidizer) and three presurant tanks mounted on the LAM deck. |
| DC power | 5859 W |
| Equipment | 12 Ku band high power transponders covering Indian main land using 140W radiatively cooled TWTAs.
12 C band high power transponders with extended coverage, covering southeast and northwest region apart from Indian main land using 63 W TWTAs |
| Design lifetime | > million years - active: 12 yrs - still active |
|
Location:
| Begin | End | Position |
| | | 93.5° E |
| July 2012 | | 93.48° E |
|
