| Designation | 28893 / 05043D |
| Launch date | 27 Oct 2005 |
| Country of origin | Iran |
| Mission | Technology |
| Perigee/Apogee | 680 km sun-synchronous |
| Inclination | |
| Period | |
| Launch vehicle | Cosmos C |
| Prime contractor | AKO Polyot |
| Platform | Sterkh (similar to Mita) |
| Mass at launch | 160 kg |
| Dry mass | |
| Dimension | 0.8 x 1.3 x 1.6 m |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime | 5 years |