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
Mission Status
Operational (nominal)
Mission Agencies
Launch Date
18 Nov 2012
Mission Links
EOL Date
Nov 2025
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.