
QZS 1 (Michibiki) [JAXA]
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.
Phase one will demonstrate the technological validation for the enhancement of GPS availability and performance and their application, using the first Quasi-Zenith Satellite (QZS 1) Michibiki. After evaluating these results, the plan moves into phase two which demonstrates the full system capability using three Quasi-Zenith Satellites, including QZS-1. JAXA is in charge of integrating the system as a whole, as well as cooperating with related research organizations to develop the High Accuracy Positioning Experiment System, the QZS Bus System and the Tracking Control System.
The QZS 1 is based on Mitsubishis ETS-8-Bus and will have a lift off weight of 4100 kg. The QZS satellites are to operate for more than 10 years.
| Nation: | Japan |
|---|---|
| Type / Application: | Navigation |
| Operator: | JAXA |
| Contractors: | Mitsubishi Electric |
| Equipment: | transponders |
| Configuration: | DS-2000 |
| Propulsion: | R-4D |
| Power: | 2 deployable solar arrays, batteries |
| Lifetime: | +10 years |
| Mass: | 4100 kg |
| Orbit: | GEO |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| QZS 1 (Michibiki) | 11.09.2010 | Ta YLP-1 | H-2A-202 | ||
| QZS 2 | Ta YLP-1 | H-2A-202 | |||
| QZS 3 | Ta YLP-1 | H-2A-202 |