| Name of Satellite, Alternate Names | BeeSat-2 (Berlin Experimental and Educational Satellite 2) |
| 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) | 555 |
| Apogee (km) | 579 |
| Eccentricity | 0.001729854403921 |
| Inclination (degrees) | 64.8 |
| Period (minutes) | 96.01 |
| Launch Mass (kg.) | 1 |
| Dry Mass (kg.) | |
| Power (watts) | |
| Date of Launch | 19-04-2013 |
| Expected Lifetime | 1 yr. |
| Contractor | Technische Universität Berlin |
| Country of Contractor | Germany |
| Launch Site | Baikonur Cosmodrome |
| Launch Vehicle | Soyuz 2.1a |
| COSPAR Number | 2013-015G |
| NORAD Number | 39136 |
| Comments | Carrying a technology experiment using gyros and sensors for precise orientation. |