Designation | 27948 / 03043A |
Launch date | 27 Sep 2003 |
Country of origin | Europe |
Mission | Telecommunications |
Geostationary orbit | 33°E |
Launch vehicle | Ariane V162 |
Begin | End | Position |
L: 27 Sep 2003 | 33°E | |
May 2014 | Jan 2018 | 31°E, inclined, Eutelsat 31A |
Out of service | Jan 2018 |
Cause | sent to junk orbit |
Prime contractor | Boeing |
Platform | BSS-376HP |
Mass at launch | 1525 kg |
Dry mass | 888 kg |
Dimension | 2.16 m diameter x 3.16 m (7.83 m deployed) |
Solar array | |
Stabilization | spin-stabilized |
DC power |
BOL:
1730 W EOL: 1600 W |
Design lifetime | 10 years |
Main transponders | 20 |
Backup transponders | |
Power | 33 W? |
Bandwidth |
16
x 36 MHz (forward link) 4 x 108 MHz (return link) |
Coverage |
4
spot beams Europe and Turkey |
EIRP max | 52 dBW |
G/T max | +8 dB/K |
Polarization | linear H/V cross-pol |
Horizontal
Uplink |
Horizontal
Downlink | Transponder |
Vertical
Downlink |
Vertical
Uplink | Bandwidth (MHz) |
14.06250 | CR | 11.01250 | 108 | ||
11.01250 | AR | 14.06250 | 108 | ||
14.18750 | BR | 11.13750 | 108 | ||
11.13750 | DR | 14.18750 | 108 | ||
11.47175 | A1 | 14.27175 | 36 | ||
14.27175 | B1 | 11.47175 | 36 | ||
11.51325 | A2 | 14.31325 | 36 | ||
14.31325 | B2 | 11.51325 | 36 | ||
11.55475 | A3 | 14.35475 | 36 | ||
14.35475 | B3 | 11.55475 | 36 | ||
11.59625 | D1 | 14.39625 | 36 | ||
14.39625 | B4 | 11.59625 | 36 | ||
11.63775 | D2 | 14.43775 | 36 | ||
14.43775 | B5 | 11.63775 | 36 | ||
11.67925 | D3 | 14.47925 | 36 | ||
14.47925 | B6 | 11.67925 | 36 | ||
13.77175 | C1 | 12.52225 | 36 | ||
13.81325 | C2 | 12.56375 | 36 | ||
13.85475 | C3 | 12.60525 | 36 | ||
13.89625 | C4 | 12.64575 | 36 | ||
13.93775 | C5 | 12.68825 | 36 | ||
13.97850 | C6 | 12.72900 | 36 |