Designation | 26298 / 00020A |
Launch date | 19 Apr 2000 |
Country of origin | United States |
Mission | Telecommunications |
Geostationary orbit | see below |
Launch vehicle | Ariane V129_v129 |
Begin | End | Position |
L: 19 Apr 2000 | Jun 2000 | 73°W |
Jun 2000 | Aug 2006 | 99°W |
Sep 2006 | Apr 2009 | 76.85°W, inclined |
Out of service | Apr 2009 |
Cause | moved to the junk orbit |
Prime contractor | Hughes |
Platform | HS-601HP |
Mass at launch | 3716 kg |
Dry mass | 1895 kg |
Mass in orbit | 2511 kg |
Dimension | stowed: 2.7 x 3.6 x 4 m |
Solar array | 26 m span, 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 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 | 45 dBW |
G/T max | 0 dB/K |
Polarization | linear H/V |
SFD | -94 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 |
11.720 | 1 | 14.020 | ||
14.040 | 2 | 11.740 | ||
11.760 | 3 | 14.060 | ||
14.080 | 4 | 11.780 | ||
11.800 | 5 | 14.100 | ||
14.120 | 6 | 11.820 | ||
11.840 | 7 | 14.140 | ||
14.160 | 8 | 11.860 | ||
11.880 | 9 | 14.180 | ||
14.200 | 10 | 11.900 | ||
11.920 | 11 | 14.220 | ||
14.240 | 12 | 11.940 | ||
11.960 | 13 | 14.260 | ||
14.280 | 14 | 11.980 | ||
12.000 | 15 | 14.300 | ||
14.320 | 16 | 12.020 | ||
12.040 | 17 | 14.340 | ||
14.360 | 18 | 12.060 | ||
12.080 | 19 | 14.380 | ||
14.400 | 20 | 12.100 | ||
12.120 | 21 | 14.420 | ||
14.440 | 22 | 12.140 | ||
12.160 | 23 | 14.460 | ||
14.480 | 24 | 12.180 |