Jcsat 11
General
| Designation | n/a |
| Launch date | 5 Sep 2007 |
| Country of origin | Japan |
| Mission | Telecommunications |
| Geostationary orbit | n/a |
| Launch vehicle | Proton #329 |
Was insured for $300 million
End of life
| Out of service | 5 Sep 2007 |
| Cause | Destroyed with the launch failure |
Technical data
Specifications
| Prime contractor | Lockheed Martin |
| Platform | A2100AX |
| Mass at launch | 4500 kg |
| Mass in orbit | |
| Dimension | |
| Solar array | |
| Stabilization | 3-axis |
| DC power | |
| Design lifetime | 15 years |
C-band
| Main transponders | 12 |
| Backup transponders | |
| Power | |
| Bandwidth | |
| Coverage | Asia-Pacific and Hawaii |
| EIRP max | |
| G/T max | |
| Polarization |
Ku-band
| Main transponders | 30 |
| Backup transponders | |
| Power | |
| Bandwidth | |
| Coverage | Japan |
| EIRP max | |
| G/T max | |
| Polarization |
This document is part of The Satellite Encyclopedia, © Tag's Broadcasting Services, all rights reserved, NO REPRODUCTION ALLOWED. Please notify any errors, omissions, etc.
V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly
V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly