Designation | 25666 / 99016A |
Launch date | 2 Apr 1999 |
Country of origin | India |
Mission | Telecommunications and meteorology |
Geostationary orbit | 83°E |
Launch vehicle | Ariane V117 |
Out of service | April 2012 |
Prime contractor | ISRO/ISAC |
Platform | INSAT2 |
Mass at launch | 2550 kg |
Mass in orbit | 1526 kg |
Dry mass | 1148 kg |
Dimension | 1.93 x 1.77 x 2.3 m |
Solar array | 24.7 m |
Stabilization | 3-axis |
DC power | 2143 W (60 Ah Nickel-Hydrogen batteries) |
Design lifetime | 12 years |
Wave bands |
0.55-0.75
µm (visible) 10.5-12.5 µm (IR) + a water vapour band |
Resolution |
visible:
2 km IR: 8 km |
Image repeat frequency | 30 minutes |
Main transponders | 15 + 2 |
Backup transponders | |
Power |
10
x 32 W 7 x 60 W |
Bandwidth |
15
x 36 MHz 2 x 72 MHz |
Coverage & EIRP max |
Quasi
global Wide beam: 36 dBW Zone: 36 dBW |
G/T max | |
Polarization | linear (uplink: H, downlink: V) |
Frequencies |
uplink:
5.850 - 6.650 GHz downlink: 3.400 - 4.200 GHz |
Horizontal
Uplink | Transponder |
Vertical
Downlink | Intelsat use | Beams (uplink/dowlink) |
6.470 | 1 | 3.445 | yes | wide/zone |
6.510 | 2 | 3.485 | yes | wide/zone |
6.550 | 3 | 3.525 | yes | wide/zone |
6.590 | 4 | 3.565 | yes | wide/zone |
6.630 | 5 | 3.605 | yes | wide/zone |
5.890 | 6 (72 MHz) | 3.665 | yes | wide/wide |
5.950 | 7 | 3.725 | wide/zone | |
5.990 | 8 | 3.765 | wide/wide | |
6.030 | 9 | 3.805 | wide/zone | |
6.070 | 10 | 3.845 | wide/wide | |
6.110 | 11 | 3.885 | wide/zone | |
6.150 | 12 | 3.925 | wide/wide | |
6.190 | 13 | 3.965 | wide/zone | |
6.230 | 14 | 4.005 | yes | wide/wide |
6.270 | 15 | 4.045 | yes | wide/wide |
6.310 | 16 | 4.085 | wide/zone | |
6.370 | 17 (72 MHz) | 4.145 | yes | wide/wide |