| Name of Satellite, Alternate Names | Vermont Lunar Cubesat |
| Country of Operator/Owner | USA |
| Operator/Owner | Vermont Technical College/University of Vermont |
| Users | Civil |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 494 |
| Apogee (km) | 504 |
| Eccentricity | 0.000727907992429757 |
| Inclination (degrees) | 40.5 |
| Period (minutes) | 94.6 |
| Launch Mass (kg.) | 1 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 19-11-2013 |
| Expected Lifetime | |
| Contractor | Vermont Technical College/University of Vermont |
| Country of Contractor | USA |
| Launch Site | Wallops Island Flight Facility |
| Launch Vehicle | Minotaur |
| COSPAR Number | 2013-064AD |
| NORAD Number | 39407 |
| Comments | Testing software and an imager for an eventual lunar orbiter/lander cubesat that will be sent to the Moon |