| Name of Satellite, Alternate Names | Falconsat-3 |
| Country of Operator/Owner | USA |
| Operator/Owner | US Air Force Academy |
| Users | Civil/Military |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 538 |
| Apogee (km) | 540 |
| Eccentricity | 0.000144738746562455 |
| Inclination (degrees) | 35.4 |
| Period (minutes) | 95.4 |
| Launch Mass (kg.) | 46 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 09-03-2007 |
| Expected Lifetime | |
| Contractor | US Air Force Academy |
| Country of Contractor | USA |
| Launch Site | Cape Canaveral |
| Launch Vehicle | Atlas 5 |
| COSPAR Number | 2007-006E |
| NORAD Number | 30776 |
| Comments | Air Force Academy’s first attempt at achieving three axis attitude determination and control (ADCS). FalconSAT-3 will carry three payloads to conduct DoD research. When primary mission completed amateur radio payload will be activated. |