HORYU-2

Japan

Spacecraft nº:

Japanese spacecraft nº: 176


Launch data:

Designation 38340 / 12025D
Launch date 17 May 2012 - 16:39 UT
Launch site Tanegashima, YLP-2
Launch vehicle  H-2A-202
Mission Civil: Technology Development
LEO Sun-Synchronous Earth orbit:
Perigee / Apogee 664 x 677 km
Eccentricity 9,23E-04
Inclination 98.18 deg
Period 98.16 min
HORYU 2

HORYU-2 nanosatellite (image credit: KIT)


Launched together with GCOM-W 1, KOMPSat 3, SDS 4

Spacecraft data:

Prime manufacturer Kyushu Institute of Technology (KIT)
Platform 
Operator Kyusyu Institute of Technology (KIT)
Mass at launch  7 kg
Dry Mass  kg
Basic shape  Cube
Dimensions 350 x 310 x 315 mm
Equipment 
Solar array Solar cells
Stabilization  
Propulsion 
DC power  
Design lifetime  1 yrs



Description:

Mission details:

External links:


Ref.: #7(JR659), #27, #226, #228 - update: 26.04.16 Home