RocketM-V
SpaceportUchinoura (Kagoshima)pad M-V
OutcomeFailurestage 1 propulsion failure / early shutdown; later stages kept firing on the wrong trajectory
Launch agencyISASJapan
Flight
- Date and time (UTC)
- February 10, 2000, 01:30
- Launch designation
- 2000-U01
- Mission
- ASTRO E
- Vehicle flight ID
- M-V-4
- Year
- Launches in 2000
Orbit and payload
- Initial apogee
- 200 km
- Payload mass to orbit
- 1.6 t
- Payloads
- 1
- GCAT launch code
- OF · S1P*
Payloads
| Payload | Designation | Owner | Mission type | Mass | Fate |
|---|---|---|---|---|---|
| ASTRO E | 2000-U01 | Institute of Space and Astronautical Sci | — | — | — |
Source: GCAT launch list and payload catalogs, Jonathan C. McDowell (CC BY 4.0). Orbit values are the initial orbit reported for the launch.