Designation | 32708 / 08011A |
Launch date | 14 Mar 2008 |
Country of origin | United States |
Mission | Telecommunications |
Geostationary orbit | see below, highly inclined |
Launch vehicle | Proton #336 |
Begin | End | Position |
L: 14 Mar 2008 | LEO | |
Jan 2009 | Jan 2013 | 34.5°E, highly inclined |
Feb 2013 | Jan 2016 | 29.5°E, highly inclined |
Apr 2016 | 18°E, highly inclined |
Prime contractor | Lockheed Martin |
Platform | A2100 |
Mass at launch | 4140 kg |
Mass in orbit | |
Dimension | |
Solar array | |
Stabilization | 3-axis |
DC power | 8.2 kW |
Design lifetime | 15 years |
Main transponders | 32 |
Backup transponders | |
Power | 150 W (TWTA) |
Bandwidth | 24 MHz |
Coverage | CONUS and certain British Overseas Territories in the Caribbean (Bermuda, Virgin Islands and Cayman Islands) Uplink is CONUS only. |
EIRP max | 54 dBW |
G/T max | 3 dB/K |
Polarization | circular L/R no cross-pol |
Frequencies: |
uplink:
17.3-17.8 GHz downlink: 12.2-12.7 GHz |
LHCP
Uplink |
LHCP
Downlink | Transponder |
RHCP
Downlink |
RHCP
Uplink |
17.31700 | 12.21700 | 1 | ||
2 | 12.23158 | 17.33158 | ||
17.34616 | 12.24616 | 3 | ||
4 | 12.26074 | 17.36074 | ||
17.37532 | 12.27532 | 5 | ||
6 | 12.28990 | 17.38990 | ||
17.40448 | 12.30448 | 7 | ||
8 | 12.31906 | 17.41906 | ||
12.43364 | 12.33364 | 9 | ||
10 | 12.34822 | 17.44822 | ||
17.46280 | 12.36280 | 11 | ||
12 | 12.37738 | 17.47738 | ||
17.49196 | 12.39196 | 13 | ||
14 | 12.40654 | 17.50654 | ||
17.52112 | 12.42112 | 15 | ||
16 | 12.43570 | 17.53570 | ||
17.55028 | 12.45028 | 17 | ||
18 | 12.46486 | 17.56486 | ||
17.57944 | 12.47944 | 19 | ||
20 | 12.49402 | 17.59402 | ||
17.60860 | 12.50860 | 21 | ||
22 | 12.52318 | 17.62318 | ||
17.63776 | 12.53776 | 23 | ||
24 | 12.55234 | 17.65234 | ||
17.66692 | 12.56692 | 25 | ||
26 | 12.58150 | 17.68150 | ||
17.69608 | 1259608 | 27 | ||
28 | 12.61066 | 17.71066 | ||
17.72524 | 12.62524 | 29 | ||
30 | 12.63982 | 17.73982 | ||
17.75440 | 12.65440 | 31 | ||
32 | 12.66898 | 17.76898 |