JCSat-16 |
Japan |
Int. spacecraft nº: |
Japanese spacecraft nº: 220 |
| Designation | 41729 / 16050A |
| Launch date | 14 Aug 2016 - 05:26 UT |
| Launch site | CC, SLC40 |
| Launch vehicle | Falcon-9 v1.2 |
| Mission | Communication |
| Geostationary orbit: | |
| Perigee / Apogee | 151 x 36183 km |
| Eccentricity | |
| Inclination | 20.9 ° |
| Period | min |
| Prime manufacturer | Space Systems/Loral (SS/L) |
| Platform | SSL-1300 |
| Operator | JSAT Corporation |
| Mass at launch | 4600 kg ? |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | Ku-band and Ka-band transponders |
| Solar array | 2 deployable solar arrays |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime | 15 yrs |
| Ref.: #7(JR729), #14 - update: 09.02.17 | Home |