Maroc-Tubsat

---

General

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

http://www.vectronic-aerospace.com/Image_Gallery/MAROC-TUBSAT/hauptteil_maroc-tubsat.html

sat-index articles

Technical data

---

---

Specifications

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.

Communications:
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

---