CEOS EO HANDBOOK – MISSION SUMMARY - HummerSat-1 -
Full Name Status Operational (nominal)
Mission Agencies CAST Launch Date 18 Nov 2012
Mission Links EOL Date Nov 2025
EO Portal Info NORAD Catalog #
International Designator
Orbit Type Inclined, non-sun-synchronous Orbit Period 92.7 minutes
Orbit Sense Ascending Orbit Inclination 97.1 deg
Orbit Altitude Orbit Longitude
Orbit LST Repeat Cycle
Objectives and Applications The overall objective of the HummerSat-1 mission is to provide a technology demonstration as well as to test observation capabilities within the spacecraft class of 80-250 kg of total mass envelop (micro/minisatellite), for a number of different missions and applications, including support scenarios of constellations and formation flight (with intersatellite crosslink, relative navigation, guidance and control).
Mission Measurements
Mission Instruments
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