ShindaiSat (Ginrei)

Japan

Spacecraft nº:

Japanese spacecraft nº: 187


Launch data:

Designation 39572 / 14009A
Launch date 27 Feb 2014 - 18:37 UT
Launch site Tanegashima, YLP-1
Launch vehicle  H-2A-202
Mission Technology
Earth orbit:
Perigee / Apogee 340 x 367 km
Eccentricity 
Inclination 65.0 °
Period 91.5 min

Launched together with: GPM-Core - STARS 2 - TeikyoSat 3 - KSAT 2 - OPUSAT - INVADER - ITF 1


Spacecraft data:

Prime manufacturer Shinshu University
Platform 
Operator Shinshu University
Mass at launch  35 kg (33 kg?)
Dry Mass  kg
Basic shape  
Dimension (m) 
Equipment 
Solar array Solar cells
Stabilization  
Propulsion None
DC power  

End of live:

Re-entered date:  24 Nov 2014
Lifetime: 


Description:


Ref.: #7(JR694) #14, #228 - update: 06.12.14 Home