![]() AubieSat-1 | |
Mission type | Technology |
---|---|
Operator | Auburn University |
COSPAR ID | 2011-061E |
SATCAT no. | 37854 |
Spacecraft properties | |
Manufacturer | Auburn University |
Start of mission | |
Launch date | October 28, 2011, 09:48:02[1] | UTC
Rocket | Delta II 7920-10C |
Launch site | Vandenberg SLC-2W |
Contractor | United Launch Alliance |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Perigee altitude | 452 kilometers (281 mi) |
Apogee altitude | 750 kilometers (470 mi) |
Inclination | 101.71 degrees |
Period | 96.58 minutes |
Epoch | July 6, 2014, 01:17:55 UTC[2] |
AubieSat-1 (OSCAR-71) is a CubeSat designed, built, and tested by undergraduate students at Auburn University. It was launched from Vandenberg Air Force Base October 28, 2011 atop a Delta II rocket. This was a multi-payload mission with five other CubeSats, M-Cubed, DICE-1, DICE-2, Explorer-1 and RAX-2.
The purpose of AubieSat-1 was to accomplish several things: