|Units or mass||2U|
|Mass in kg||2.603 kg|
|Status||Reentry 2013-08-06. Was operational until 2013-07-15. For the last 20 days only beacons.|
|Deployer||J-SSOD (JEM Small Satellite Orbital Deployer)|
|Deployment||Deployed from ISS on 2012-10-04|
|Entity||Academic / Education|
Demonstrate technologies for larger satellites including CMOS and CCD sensors.
Demonstration of new electronics or mechanism usable for 50-kg microsatellites, which are CMOS color sensor, CCD color sensor, CCD star sensor, and film deployment mechanism.
|Failure cause||Assumed that the frequency lock function of on-board receiver was easily terminated because the satellite rotation speed was fast.|