Designation | n/a |
Launch date | 1 Feb 2013 |
Country of origin | International |
Mission | Telecommunications |
Geostationary orbit | 55.5°W |
Launch vehicle | Zenit Sea Launch |
Out of service | 1 Feb 2013 |
Cause | launch failure |
Prime contractor | Boeing |
Platform | HS702MP |
Mass at launch | 5450 kg |
Dry mass | |
Dimension | |
Solar array | |
Stabilization | 3-axis |
DC power | |
Design lifetime | 15 years |
Main transponders | 20 |
Backup transponders | |
Power | |
Bandwidth | 25 kHz |
Coverage | |
EIRP max | |
G/T max | |
Polarization | |
Frequencies |
243.52-268.16
MHz 292.835-317.33 MHz |
Main transponders | 20 |
Backup transponders | |
Power | |
Bandwidth |
16
x 36 MHz 4 x 72 MHz |
Coverage | America and Europe |
EIRP max | 39 dBW |
G/T max | |
Polarization | linear H/V |
Frequencies |
uplink:
5.925-6.425 GHz downlink: 3.700-4.200 GHz |
Main transponders | 19 (24 in 36-MHz equivalent) |
Backup transponders | |
Power | |
Bandwidth | 27, 36, 54, 72, 77 MHz |
Coverage |
North
Atlantic Andean/Mexico Brazil |
EIRP max | |
G/T max | |
Polarization | linear H/V |
Frequencies |
uplink:
14.0-14.5 GHz downlink: 11.45-11.70 GHz & 11.70-12.2 GHz & 12.5-12.75 GHz |