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. |