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).
Full Name
HummerSat-1
Mission Status
Mission complete
Mission Agencies
Launch Date
18 Nov 2012
Mission Links
EOL Date
01 Nov 2024
Orbit Type
Inclined, non-sun-synchronous
Orbit Period
92.7 minutes
Orbit Sense
Ascending
Orbit Inclination
97.1 deg
Orbit Altitude
Orbit Longitude
NORAD Catalog #
International Designator
No IDN OpenSearch datasets found.