Designation | 27714 / 03013A |
Launch date | 9 Apr 2003 |
Country of origin | India |
Mission | Telecommunications and meteorology |
Geostationary orbit | see below |
Launch vehicle | Ariane V160 |
Begin | End | Position |
L: Apr 2003 | Nov 2016 | 93.5°E |
Out of service | Nov 2016 |
Cause | EOL |
Prime contractor | ISRO |
Platform | INSAT 3 |
Mass at launch | 2950 kg |
Dry mass | 1350 kg |
Dimension | 2.8 x 1.7 x 2 m (24.4 m span deployed) |
Solar array | single panel |
Stabilization | 3-axis |
DC power | EOL: 3230 W |
Design lifetime | 12 years |
Main transponders | 12 + 6 (extended) |
Backup transponders | |
Power | |
Bandwidth | 36 MHz |
Coverage & EIRP max |
Quasi
global (9 transp) Wide beam: 38 dBW (9 transp) India (India, Bengladesh, Bhutan, Nepal): 37 dBW |
G/T max | -5 |
Polarization | H/V crosspol |
Frequencies |
extended:
uplink: 6.755-6.995 GHz;downlink: 4.530-4.770 GHz standard: uplink: 5.950-6.410 GHz; downlink: 3.725-4.185 GHz |
Horizontal Uplink |
Horizontal Downlink | Channel |
Vertical Downlink |
Vertical Uplink |
5.970 | 1 | 3.745 | ||
6.010 | 2 | 3.785 | ||
6.050 | 3 | 3.825 | ||
6.090 | 4 | 3.865 | ||
6.130 | 5 | 3.905 | ||
6.170 | 6 | 3.945 | ||
6.210 | 7 | 3.985 | ||
6.250 | 8 | 4.025 | ||
6.290 | 9 | 4.065 | ||
6.330 | 10 | 4.105 | ||
6.370 | 11 | 4.145 | ||
6.410 | 12 | 4.185 | ||
6.775 | 4.550 | |||
6.815 | 4.590 | |||
6.855 | 4.630 | |||
6.895 | 4.670 | |||
6.935 | 4.710 |
Main transponders | 6 |
Backup transponders | |
Power | |
Bandwidth | 36 MHz |
Coverage | India, Bengladesh, Bhutan, Nepal |
EIRP max | 47.5 dBW |
G/T max | |
Polarization | H/V crosspol |
Frequencies |
uplink:
14.250-14.500 GHz downlink: 11.450-11.700 GHz |