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Mission type | Technology |
---|---|
Operator | Osaka Prefecture University |
COSPAR ID | 2014-009D |
SATCAT no. | 39575 |
Website | www |
Spacecraft properties | |
Spacecraft type | 1U CubeSat |
Manufacturer | Osaka Prefecture University |
Launch mass | 1.4 kilograms (3.1 lb) |
Start of mission | |
Launch date | 27 February 2014, 18:37 UTC [1] |
Rocket | H-IIA 202 |
Launch site | Tanegashima Yoshinobu 1 |
Contractor | Mitsubishi |
End of mission | |
Decay date | 24 July 2014 |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 383 kilometres (238 mi) |
Apogee altitude | 389 kilometres (242 mi) |
Inclination | 65 degrees |
Period | 92.27 minutes |
Epoch | 28 February 2014 [2] |
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