QZS 1 (Michibiki)

 

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