Satellite Hodoyoshi-3 of University of Tokyo and NESTRA

Name of Satellite, Alternate Names Hodoyoshi-3
Country of Operator/Owner Japan
Operator/Owner University of Tokyo and NESTRA
Users Government
Purpose Technology Development
Class of Orbit LEO
Type of Orbit Sun-Synchronous
Longitude of GEO (degrees) 0
Perigee (km) 613
Apogee (km) 666
Eccentricity 0.0037805834938298
Inclination (degrees) 97.98
Period (minutes) 97.51
Launch Mass (kg.) 60
Dry Mass (kg.)
Power (watts) 50
Date of Launch 19-06-2014
Expected Lifetime
Contractor University of Tokyo
Country of Contractor Japan
Launch Site Dombarovsky Missile Base
Launch Vehicle Dnepr
COSPAR Number 2014-033F
NORAD Number 40015
Comments Accelerate the technology development and practical utilization of micro/nano-satellites.


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