| Designation | 26559 / 00060A |
| Launch date | 6 Oct 2000 |
| Country of origin | Japan |
| Mission | Telecommunications |
| Geostationary orbit | 110°E |
| Launch vehicle | Ariane V133 |
| Prime contractor | Lockheed Martin |
| Platform | A2100AX |
| Mass at launch | 3531 kg |
| Mass in orbit | 2100 kg |
| Dry mass | 1669 kg |
| Dimension | 8.3 m wide deployed |
| Solar array | 26.4 m span |
| Stabilization | 3-axis |
| DC power | EOL: 8300 W |
| Design lifetime | 15 years |
| Main transponders | 24 (used by pairs) |
| Backup transponders | |
| Power | 120 W |
| Bandwidth | 36 MHz |
| Coverage | Japan only |
| EIRP max | 57 dBW |
| G/T max | |
| Polarization | circular |
|
LHCP
Downlink | Transponder |
RHCP
Downlink |
| 12.271 | 1 | |
| 2 | 12.291 | |
| 12.311 | 3 | |
| 4 | 12.331 | |
| 12.351 | 5 | |
| 6 | 12.371 | |
| 12.391 | 7 | |
| 8 | 12.411 | |
| 12.431 | 9 | |
| 10 | 12.451 | |
| 12.471 | 11 | |
| 12 | 12.491 | |
| 12.511 | 13 | |
| 14 | 12.531 | |
| 12.551 | 15 | |
| 16 | 12.571 | |
| 12.591 | 17 | |
| 18 | 12.611 | |
| 12.631 | 19 | |
| 20 | 12.651 | |
| 12.671 | 21 | |
| 22 | 12.691 | |
| 12.711 | 23 | |
| 24 | 12.731 |