VEP-3 |
Japan |
Spacecraft n°: |
Japanese satellite n°: 100 |
| Designation | 27368 / 02003B |
| Launch date | 04 Feb 2002 - 02:45 UT |
| Launch site | Tanegashima |
| Launch vehicle | H-2A 2024 (#8) |
| Mission | |
| Earth orbit: | |
| Perigee / Apogee | 986 / 33758 km |
| Inclination | 23.6° |
| Period | min |
| Prime contractor | |
| Customer | |
| Platform | |
| Mass at launch | kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime |