| ALMASat-1 | |
| Mission Type: | Technology |
| Operator: | University of Bologna |
| Cospar Id: | 2012-006B |
| Satcat: | 38078 |
| Launch Mass: | 12.5kg (27.6lb) |
| Dimensions: | cube |
| Launch Date: | UTC |
| Launch Site: | Kourou ELA-1 |
| Launch Contractor: | Arianespace |
| Decay Date: | 25 April 2020 |
| Orbit Epoch: | 19 December 2013, 04:49:04 UTC[1] |
| Orbit Reference: | Geocentric |
| Orbit Regime: | Low Earth |
| Orbit Periapsis: | 311km (193miles) |
| Orbit Apoapsis: | 1250km (780miles) |
| Orbit Inclination: | 69.5 degrees |
| Orbit Period: | 100.32 minutes |
| Apsis: | gee |
ALMASat-1 (ALma MAter SATellite) was a micro satellite developed by University of Bologna for demonstrative purposes to benefit Earth observation missions. The project was funded by Italian Ministry of Research.[2]
The satellite was made from high quality aluminium and reinforced with eight stainless steel plates. Solar cells were mounted on four sides of satellite for providing the power required for satellite operation.
The work on development of ALMASat was started in 2003. It was expected to be launched into orbit on a Dnepr rocket. Later it was launched by Vega launch vehicle with other satellites on board.
The ALMASat-1 was a microsatellite having a cuboidal structure, meant for a demo purpose, it accommodated payloads of different sizes and power requirements.The main purpose of ALMASat-1 was to test the 3-axis pointing accuracy for the future satellite launches.[3]
ALMASAT-1 was launched by Vega launch system on February 13, 2012, from Kourou, French Guiana.
ALMASAT-1 decayed from orbit 25 April 2020.