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Hodoyoshi 3 & 4


Designation #3: 40015 / 14033F
#4: 40011 / 14033B
Launch date 19 Jun 2014
Country of origin Japan
Mission Remote sensing
Perigee/Apogee 615/670 km
Inclination 98°
Period 97 min
Launch vehicle Dnepr #20

Hodoyoshi 3 has medium resolution: 40 m to 200 m
Hodoyoshi 4 has high resolution: 5 m

External resources


sat-index articles

n2yo.com tracking

sat-index articles

n2yo.com tracking

Technical data


Prime contractor University of Tokyo
Platform Axelspace
Mass at launch 60 kg
Dry mass  
Solar array 2 panels
Stabilization 3-axis
DC power 100 W
Design lifetime  

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