Origamisat 1

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

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General

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

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End of life

Out of service
Cause
Decay	30 Apr 2022

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External resources

http://origami.titech.ac.jp/

sat-index articles

n2yo.com tracking

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