Table 1
QZS-1 mission parameters (ILRS 2017a)

Parameter Value
Launch date 2010-09-11
Sponsor Cabinet Office, Government of Japan
Expected life 12 years
Primary applications Technology demonstration for satellite navigation
Primary SLR applications Calibration of GPS orbits
NP bin size 300 sec
Altitude 32,000-40,000 km
Inclination 45°
Eccentricity 0.075