Himawari-8

Japan

Spacecraft nº:

Japanese spacecraft nº: 201


Launch data:

Designation 40267 / 14060A
Launch date 07 Oct 2014 - 05:16 UT
Launch site Tanegashima, YLP-1
Launch vehicle  H-2A-202
Mission Meteorology, Communication
Geostationary orbit on Oct 15:
Perigee / Apogee 35756 x 35813 km
Eccentricity 
Inclination  0.01°
Period 1436.08 min
Himawari 8



Spacecraft data:

Prime manufacturer Mitsubishi Electric (prime), Boeing
Platform DS-2000 bus
Operator Japanese Ministry of Transport Civil Aviation Bureau & Meteorological Agency
Mass at launch  ~3500 kg
Dry Mass 1300 kg
Basic shape  
Dimension (m) 
Equipment AHI, SEDA, DCS
Solar array Deployable solar array
Stabilization  
Propulsion 
DC power  
Design lifetime  15 years (meteorological mission 8 years)

Location:

DatePositionRemarks
 Dec 2014  140.8° E 



Description:

Mission details:

External links:


Ref.: #7(JR703,706), #14, #207, #228 - update: 15.01.15 Home