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Designation 39402 / 13064Y
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 University of Florida.

Will demonstrate rapid retargeting and precision pointing maneuvers using miniaturized control moment gyroscopes.

1U cubesat.

Downlink: 437.385 MHz

End of life

Decay 13 Dec 2015

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