Last modification: March 7, 2006
| Launch date | |||
| Launch
window: Status: |
February
18, 2006 - 0627 UTC. Completed. |
||
| Launch site | |||
| Location: Launch complex: |
Tanegashima
Space Centre (Japan) Yoshinobu Launch Complex |
||
| Launch vehicle | |||
|
Version: |
H-2A/2024 [Standard H-2A 2nd stage] 5S Mitsubishi Heavy Industries Ltd. Rocket System Corp. (RSC) F9 |
||
| Performance | |||
| Targeted
orbit: Overall lift-off mass: Total payload mass: |
Geostationary
Transfer Orbit About 354,000 kg About 3,500 kg (est.) |
||
| Milestones | |||
|
|||
| Payload | ||||
| Payload designation | Launch customer | Launch contract |
Launch mass
|
Launch adapter
|
| MT-Sat 2 | MLIT | Feb.
2003 |
3,000
kg |
n.a. |
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