| Name of Satellite, Alternate Names | BeeSat-1 (Berlin Experimental and Educational Satellite 1) |
| Country of Operator/Owner | Germany |
| Operator/Owner | Institut für Luft- und Raumfahrt |
| Users | Civil |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 709 |
| Apogee (km) | 718 |
| Eccentricity | 0.000635279169901885 |
| Inclination (degrees) | 98.3 |
| Period (minutes) | 99 |
| Launch Mass (kg.) | 1 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 23-09-2009 |
| Expected Lifetime | 1 yr. |
| Contractor | Technische Universität Berlin |
| Country of Contractor | Germany |
| Launch Site | Sriharikota Launch Station |
| Launch Vehicle | PSLV |
| COSPAR Number | 2009-051C |
| NORAD Number | 35933 |
| Comments | Verify the behavior of new micro reaction wheels for picosatellites. |