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Designation 27004 / 01056D
Launch date 10 Dec 2001
Country of origin Morocco
Mission Remote sensing
Perigee/Apogee 986/1014 km sun-synchronous
Inclination 99.7°
Period 105 min
Launch vehicle Zenit #35

Cooperation between CRTS Morocco and the Institut für Luft-und Raumfahrttechnik in Berlin ( Tubsat program).

External resources


sat-index articles

Technical data


Prime contractor Technical University of Berlin
Platform Tubsat C
Mass at launch 47 kg
Mass in orbit  
Dimension 32 x 34 x 36.2 cm
Solar array 4 solar panels, 14 W each
Stabilization 3-axis
DC power  
Design lifetime  

Payload provided by CRTS. 300 m resolution sensor + store and forward communication.

144.1 (143.625 initially planned) MHz, Modulation FFSK, 1200/2400 Baud, 3.5 W RF output
436.075 MHz, Modulation FFSK, 1200/2400 Baud, 5.0 W RF output
2208.0 MHz, Modulation BPSK, FEC, max 250 kBaud, 2.0 W RF output

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