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Almasat 1


ALma MAter SATellite

General


Designation 38078 / 12006B
Launch date 13 Feb 2012
Country of origin Italy
Mission Technology
Perigee/Apogee 322/1447 km
Inclination 69.5°
Period 102.5 min
Launch vehicle Vega #1

For the University of Bologna.

To demonstrate a new satellite bus.

External resources


http://www.almasat.unibo.it/02_projects/almasat-1/almasat1.htm

sat-index articles


n2yo.com tracking


Technical data



Specifications


Prime contractor University of Bologna
Platform Almasat bus
Mass at launch 12.5 kg
Dry mass  
Dimension 30 cm cube
Solar array  
Stabilization 3-axis
DC power  
Design lifetime  

Downlink: 437.465 MHz 1200bps FSK and 2407.850 MHz

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