H3-22 | Michibiki 5 (QZS-5)
Mitsubishi Heavy IndustriesYoshinobu Launch Complex LP-2 — Tanegashima Space Center, Japan
Either the launch vehicle did not reach orbit, or the payload(s) failed to separate.
mission
- Name
- Michibiki 5 (QZS-5)
- Type
- Navigation
- Target orbit
- Geosynchronous Transfer Orbit (GSTO)
QZSS (Quasi Zenith Satellite System) is a Japanese satellite navigation system operating from inclined, elliptical geosynchronous orbits to achieve optimal high-elevation visibility in urban canyons and mountainous areas. The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation. The navigation system objective is to broadcast GPS-interoperable and augmentation signals as well as original Japanese (QZSS) signals from a three-spacecraft constellation in inclined, elliptical geosynchronous orbits.
schedule
- NET (no earlier than)
- Window opens
- Window closes
- Last updated
- Fail reason
- 2nd stage liquid hydrogen tank pressure abnormally start decreasing after fairing separation, leading up to 2nd stage 1st burn 27 seconds longer than planned & engine shutting down 1 second into 2nd burn. Payload stranded in LEO and re-entered shortly after.
vehicle & provider
- Rocket
- H3-22
- Family
- H3
- Variant
- 22
- Provider
- Mitsubishi Heavy Industries
- Type
- Commercial
- Country
- JPN
webcasts
launch site
- Pad
- Yoshinobu Launch Complex LP-2
- Location
- Tanegashima Space Center, Japan
- Country
- JPN
- Timezone
- Asia/Tokyo
- Coordinates
- 30.4009, 130.9756