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Origamisat 1

ORganisatIon of research Group on Advanced deployable Membrane structures for Innovative space science
FO-98, Fuji Oscar 98


Designation 43933 / 19003B
Launch date 18 Jan 2019
Country of origin Japan
Mission Technology
Perigee/Apogee 497 / 520 km
Inclination 97.3°
Period 94.7 min
Launch vehicle Epsilon #4

Project from Tokyo institute of technology. The satellite has a deployable membrane structure (1.4m²) experiment and a 5.8 GHz communication payload.
3U cubesat, 4 kg

Amateur radio on 437.505 nad 5840 MHz down, 437.497 MHz up

End of life

Out of service  
Decay 30 Apr 2022

External resources


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