Tsubasa |
Japan |
Spacecraft n°: |
Japanese satellite n°: 99 |
| Designation | 27367 / 02003A |
| Launch date | 04 Feb 2002 - 02:45 UT |
| Launch site | Tanegashima |
| Launch vehicle | H-2A 2024 (#8) |
| Mission | Technology |
| Earth orbit on: | |
| Perigee/Apogee | 500 / 36000 km |
| Inclination | |
| Period | |
| Prime contractor | NEC |
| Platform | |
| Mass at launch | 449 kg |
| Mass in orbit | |
| Dimension | box-shaped, 3.3 x 1.6 m |
| Solar array | |
| Stabilization | spin-stabilized |
| DC power | 900 W |
| Design lifetime | 1 year |