Designation | 27954 / 03044A |
Launch date | 1 Oct 2003 |
Country of origin | United States |
Mission | Telecommunications |
Geostationary orbit | see below |
Launch vehicle | Zenit Sea Launch #11 |
Begin | End | Position |
L: | Nov 2003 | 144.5°W |
Jan 2004 | Oct 2023 | 127°W |
Nov 2023 | 150°W |
Prime contractor | Boeing |
Platform | HS-601HP |
Mass at launch | 4090 kg |
Mass in orbit | 2630 kg |
Dimension | |
Solar array | dual junction |
Stabilization | 3-axis |
DC power |
BOL:
9.9 kW EOL: 8.6 kW |
Design lifetime | 15 years |
Main transponders | 24 |
Backup transponders | 8 |
Power | 40 W (LTWTAs) |
Bandwidth | |
Coverage | 127°W: North America, Central America, Alaska and Hawaii |
EIRP max | 40 dBW |
G/T max | 3 dB/K |
Polarization | linear H/V cross-pol |
Main transponders | 24 |
Backup transponders | 8 |
Power | 108 W (LTWTAs) |
Bandwidth | 36 MHz |
Coverage | 127°W: Hawaii, Alaska, Conus, par of the Caribbean |
EIRP max | 48 dBW |
G/T max | 2 dB/K |
Polarization | linear H/V |
Frequencies |
uplink:
14.0-14.5 GHz downlink: 11.7-12.2 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 |