Safir program |
Germany |
| Perigee/Apogee | 678/696 km |
| Inclination | 98.4° |
| Period | 98 min |
| Uplinks | 401 MHz |
| Downlinks | 400 MHz |
| Prime contractor | |
| Platform | |
| Mass at launch | 55 kg |
| Mass in orbit | |
| Length | 45 cm |
| Width | 45 cm |
| Height | 45 cm |
| Stabilization | |
| DC power | |
| Design lifetime |