| Name of Satellite, Alternate Names | Maroc Tubsat |
| Country of Operator/Owner | Morocco/Germany |
| Operator/Owner | CTRS Morocco/Institut für Luft-und Raumfahrttechnik (Berlin) |
| Users | Government |
| Purpose | Technology Development |
| Class of Orbit | LEO |
| Type of Orbit | Sun-Synchronous |
| Longitude of GEO (degrees) | 0 |
| Perigee (km) | 984 |
| Apogee (km) | 1014 |
| Eccentricity | 0.00203555434930113 |
| Inclination (degrees) | 99.2 |
| Period (minutes) | 105.1 |
| Launch Mass (kg.) | 47 |
| Dry Mass (kg.) | |
| Power (watts) | 56 |
| Date of Launch | 10-12-2001 |
| Expected Lifetime | 2-3 yrs. |
| Contractor | CRTS Morocco/Institut für Luft-und Raumfahrttechnik |
| Country of Contractor | Morocco/Germany |
| Launch Site | Baikonur Cosmodrome |
| Launch Vehicle | Zenit |
| COSPAR Number | 2001-056D |
| NORAD Number | 27004 |
| Comments | Test three-dimensional attitude control system for future remote sensing; currently used for ice observation in Arctic. |