H-IIA 202 | Michibiki 4 (QZS-4)
Mitsubishi Heavy IndustriesYoshinobu Launch Complex LP-1 — Tanegashima Space Center, Japan
The launch vehicle successfully inserted its payload(s) into the target orbit(s).
mission
- Name
- Michibiki 4 (QZS-4)
- Type
- Navigation
- Target orbit
- Geosynchronous Transfer Orbit (GSTO)
The Quasi-Zenith Satellite System (QZSS) is a three-satellite regional time transfer system and the satellite-based augmentation system for the GPS that would be receivable within Japan. The primary purpose of QZSS is to increase the availability of GPS in Japan's numerous urban canyons, where only satellites at very high elevation can be seen. A secondary function is performance enhancement, increasing the accuracy and reliability of GPS derived navigation solutions. A single satellite weighs about 4000 kg, has an expected lifetime of 15 years and is put in a elliptical, highly inclined geosynchronous orbit.
schedule
- NET (no earlier than)
- Window opens
- Window closes
- Last updated
vehicle & provider
- Rocket
- H-IIA 202
- Family
- H-II
- Variant
- 202
- Provider
- Mitsubishi Heavy Industries
- Type
- Commercial
- Country
- JPN
webcasts
launch site
- Pad
- Yoshinobu Launch Complex LP-1
- Location
- Tanegashima Space Center, Japan
- Country
- JPN
- Timezone
- Asia/Tokyo
- Coordinates
- 30.4008, 130.9777