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Mission type | Technology demonstrator |
---|---|
Operator | NICT [1] |
COSPAR ID | 2014-029C |
SATCAT no. | 39768 |
Website | Official page (Japanese) |
Spacecraft properties | |
Manufacturer | Advanced Engineering Services Co., Ltd. [1] |
Launch mass | 48 kg (106 lb) |
Dimensions | 496 mm × 495 mm × 485 mm (19.5 in × 19.5 in × 19.1 in) |
Power | 120W |
Start of mission | |
Launch date | 24 May 2014 |
Rocket | H-IIA 202 |
Launch site | Tanegashima, LA-Y |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun Synchronous |
Eccentricity | 0.0013 |
Perigee altitude | 629.8 km |
Apogee altitude | 647.4 km |
Inclination | 97.9 |
Period | 97.5 min |
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