 Launch cancel Kourou |
 Headquarter cancel Paris |
JCSat 8 |
Japan |
Spacecraft n°: |
Japanese satellite n°: 102 |
| Designation | 27399 / 02015A |
| Launch date | 29 Mar 2002 - 01:29 UT |
| Launch site | Ko, ELA-2 (ELA-3?) |
| Launch vehicle | Ariane-44L (V149) |
| Mission | Communications |
| Geostationary orbit on: | |
| Perigee / Apogee | km |
| Eccentricity | |
| Inclination | deg |
| Period | min |
| Location | 154°E |
| Prime contractor | Hughes |
| Platform | HS-601 |
| Mass at launch | 2600 kg |
| Mass in orbit | 1460 kg |
| Dry mass | 1200 kg |
| Dimension | 3.6 x 2.7 x 4.3 m (deployed: 7.6 x 4.3 x 21 m) |
| Solar array | |
| Stabilization | 3-axis |
| DC power | EOL: 3700 W |
| Design lifetime | 11 years |
| Main transponders | 16 |
| Backup transponders | |
| Power | 34 W |
| Bandwidth |
5
x 54 MHz 11 x 36 MHz |
| Coverage | Japan, East Asia, Oceania and Hawaii |
| EIRP max | |
| G/T max | |
| Polarization | linear H/V |
| Main transponders | 16 |
| Backup transponders | |
| Power | 120 W |
| Bandwidth | 57 MHz |
| Coverage | Japan |
| EIRP max | |
| G/T max | |
| Polarization | linear H/V |
|
Launch cancel Kourou |
Headquarter cancel Paris |
| Ref.: #7, #15, #415 - update: 05.11.19 | Home |