JCSat-9 |
Japan |
Spacecraft n°: |
Japanese satellite n°: 130 |
| Designation | 29045 / 06010A |
| Launch date | 12 Avr 2006 - 23:30 UT |
| Launch site | Odyssey, POR |
| Launch vehicle | Zenith-3SL |
| Mission | Commsat |
| Geostationary orbit: | |
| Perigee / Apogee | 35781 x 35792 km |
| Inclination | 0.0° |
| Period | 1436.1 min |
| Prime contractor | |
| Operator | |
| Platform | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |