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Designation 39395 / 13064R
Launch date 20 Nov 2013
Country of origin United States
Mission Technology
Perigee/Apogee 500 km
Inclination 40.5°
Period 94.5 min
Launch vehicle Minotaur #15

From Saint Louis University

Will capture payload post-separation sequence in longwave infrared. The results will automatically identify radiation effects on the payload and provide beneficial data to be used on future missions.

1U cubesat
Downlink: 437.290 MHz

End of life

Decay 4 Feb 2016

External resources


sat-index articles

n2yo.com tracking

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