Designation | 26056 / 00002A |
Launch date | 25 Jan 2000 |
Country of origin | United States |
Mission | Telecommunications |
Geostationary orbit | 123°W |
Launch vehicle | Ariane V126 |
Out of service | Jun 2008 |
Cause | Moved to the junk orbit |
Prime contractor | Hughes |
Platform | HS-601HP |
Mass at launch | 3651 kg |
Mass in orbit | 2137 kg |
Dry mass | 1987 kg |
Dimension | 2.7 x 3.6 x 4 m |
Solar array | 26 m span, dual-junction gallium arsenide |
Stabilization | 3-axis |
DC power |
BOL:
8800 W EOL: 7800 W |
Design lifetime | 15 years |
Main transponders | 24 |
Backup transponders | 4 |
Power | 40 W |
Bandwidth | 36 MHz |
Coverage | North America |
EIRP max | 41.5 dBW |
G/T max | -1 dB/K |
Polarization | linear H/V |
SFD | -94 dBW/m² (at 0 G/T & 0 dB attenuation) |
Frequencies |
Uplink:
5.925 - 6.425 GHz Downlink: 3.700 - 4.200 GHz |
Main transponders | 24 |
Backup transponders | 4 |
Power | 108 W |
Bandwidth | 36 MHz |
Coverage | North America |
EIRP max | 47.5 dBW |
G/T max | 0 dB/K |
Polarization | linear H/V |
SFD | -95 dBW/m² (at 0 G/T & 0 dB attenuation) |
Frequencies |
Uplink:
14.000 - 14.500 GHz Downlink: 11.700 - 12.200 GHz |
Horizontal Uplink |
Horizontal Downlink | Transponder |
Vertical Downlink |
Vertical Uplink |
14.020 | 1 | 11.720 | ||
11.740 | 2 | 14.040 | ||
14.060 | 3 | 11.760 | ||
11.780 | 4 | 14.080 | ||
14.100 | 5 | 11.800 | ||
11.820 | 6 | 14.120 | ||
14.140 | 7 | 11.840 | ||
11.860 | 8 | 14.160 | ||
14.180 | 9 | 11.880 | ||
11.900 | 10 | 14.200 | ||
14.220 | 11 | 11.920 | ||
11.940 | 12 | 14.240 | ||
14.260 | 13 | 11.960 | ||
11.980 | 14 | 14.280 | ||
14.300 | 15 | 12.000 | ||
12.020 | 16 | 14.320 | ||
14.340 | 17 | 12.040 | ||
12.060 | 18 | 14.360 | ||
14.380 | 19 | 12.080 | ||
12.100 | 20 | 14.400 | ||
14.420 | 21 | 12.120 | ||
12.140 | 22 | 14.440 | ||
14.460 | 23 | 12.160 | ||
12.180 | 24 | 14.480 |