CEOS EO HANDBOOK – MISSION SUMMARY - ALMASat-1 -
Full Name Alma Mater Satellite-1 Status Mission complete
Mission Agencies University of Bologna Launch Date 14 Feb 2012
Mission Links EOL Date 14 Feb 2017
EO Portal Info NORAD Catalog #
International Designator
Orbit Type Highly elliptical Orbit Period 103 minutes
Orbit Sense N/A Orbit Inclination 69.5 deg
Orbit Altitude 1450 km Orbit Longitude
Orbit LST Repeat Cycle
Objectives and Applications ALMASat is a microsatellite project at the II School of Engineering at the University of Bologna, Forlì campus, Italy. The project started in 2003, involving students, researchers, and faculty of the Engineering School as well as cooperations with external institutions and industry. Basic requirements call for a low-cost and reliable mission with simple design goals
Mission Measurements
Mission Instruments
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