Designation | 25638 / 99009A |
Launch date | 26 Feb 1999 |
Country of origin | Arab States |
Mission | Telecommunications |
Geostationary orbit | see below |
Launch vehicle | Ariane V116 |
Begin | End | Position |
L: 26 Feb 1999 | Mar 1999 | 23.7°E (tests) |
Apr 1999 | Nov 2008 | 26°E |
Nov 2008 | Aug 2009 | 30.5°E, inclined |
Out of service | Aug 2009 |
Cause | Moved to the junk orbit |
Prime contractor | Aerospatiale |
Platform | Spacebus-3000B |
Mass at launch | 2708 kg |
Mass in orbit | 1646 kg |
Dry mass | 1200 kg |
Dimension | 3.83 x 3.35 x 2.26 m at launch |
Solar array | 29 m |
Stabilization | 3-axis |
DC power | 6400 W |
Design lifetime | 12 years |
Main transponders | 20 |
Backup transponders | 8 |
Power | (TWTA) |
Bandwidth | 34 MHz |
Coverage | |
EIRP max | 48.5 dBW |
G/T max | 0.2 dB/K |
Polarization | linear H/V |
Frequencies |
Uplink:
17.3-18.1 GHz Downlink: 11.7-12.5 GHz |
Horizontal
Uplink |
Horizontal
Downlink | Channel |
Vertical
Downlink |
Vertical
Uplink |
11.72748 | 1 | 17.32748 | ||
17.34666 | 2 | 11.74666 | ||
11.76584 | 3 | 17.36584 | ||
17.38502 | 4 | 11.78502 | ||
11.80420 | 5 | 17.40420 | ||
17.42338 | 6 | 11.82338 | ||
11.84256 | 7 | 17.44256 | ||
17.46174 | 8 | 11.86174 | ||
11.88092 | 9 | 17.48092 | ||
17.50010 | 10 | 11.90010 | ||
11.91928 | 11 | 17.51928 | ||
17.53848 | 12 | 11.93848 | ||
11.95764 | 13 | 17.55764 | ||
17.57682 | 14 | 11.97682 | ||
11.99600 | 15 | 17.5960 | ||
17.61518 | 16 | 12.01518 | ||
12.03436 | 17 | 17.63436 | ||
17.65354 | 18 | 12.05354 | ||
12.07272 | 19 | 17.67272 | ||
17.69190 | 20 | 12.09190 |