Designation | 35696 / 09042A |
Launch date | 11 Aug 2009 |
Country of origin | China |
Mission | Telecommunications |
Geostationary orbit | 100.5°E |
Launch vehicle | Proton #349 |
Prime contractor | SS/L |
Platform | FS1300 |
Mass at launch | 3760 kg |
Dry mass | |
Dimension | |
Solar array | |
Stabilization | 3-axis |
DC power | |
Design lifetime | 15-years |
Main transponders | 26 |
Backup transponders | |
Power | |
Bandwidth | |
Coverage | Large Asia (almost global except south western Indian Ocean) |
EIRP max | |
G/T max | |
Polarization |
Main transponders | 14 |
Backup transponders | |
Power | |
Bandwidth | |
Coverage |
East
Asia (Japan, China, north of India & Pakistan) South Asia (Turkey; Middle East, most of central Asia, India) Steerable |
EIRP max | |
G/T max | |
Polarization |