| Name of Satellite, Alternate Names | ALiCE (AFIT LEO iMESA CNT E) |
| Country of Operator/Owner | USA |
| Operator/Owner | US Air Force Institute of Technology |
| Users | Military |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 443 |
| Apogee (km) | 886 |
| Eccentricity | 0.0314876679223825 |
| Inclination (degrees) | 120.3 |
| Period (minutes) | 98 |
| Launch Mass (kg.) | 5 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 06-12-2013 |
| Expected Lifetime | |
| Contractor | US Air Force Institute of Technology |
| Country of Contractor | USA |
| Launch Site | Vandenberg AFB |
| Launch Vehicle | Atlas 5 |
| COSPAR Number | 2013-072F |
| NORAD Number | 39467 |
| Comments | Testing a potential lightweight propulsion system for microsatellites based on an array of advanced carbon nanotubes for accelerating ions. |