Official name TEIKYOSAT-4 (OORURI)
Alternative name Oruri
Cospar ID 2021-102B
Norad ID 49396
Launch date 2021-11-09
Launch site KSCUT
Launch vehicle Epsilon (2) CLPS
Country/Organization Japan
Type application Life science
Operator Teikyo University
RCS size MEDIUM
Decay date ON ORBIT
Period (min) 95.74
Inclination (deg) 97.46
Perigee (km) 544
Apogee (km) 565
Eccentricity 0.0189359783588819
Mean motion (revs. per day) 15.0407353248381
Semi-Major axis (km) 6932.635
Raan (deg) 175.2375
Arg of perigee (deg) 58.1269
Shape Box
Mass (kg) 52
Height (m) 0.55
Width (m) 0.55
Depth (m) 0.55
Span (m^2) 0.55
Contractors Teikyo University
Propulsion ?
Power Solar cells, batteries

TeikyoSat 4 or Ooruri will test a new satellite platform capable of automatically performing biological, mechanical engineering or physics experiments using space microgravity.

It was launched on 9 November 2021 on an Epsilon (2) CLPS rocket.

Satellite COSPAR Date LS Launch Vehicle Remarks
TEIKYOSAT-4 (OORURI) 2021-102B 2021-11-09 KSCUT Epsilon (2) CLPS with RAISE 2, Hibari, Z-Sat, DRUMS, ASTERISC, NanoDragon, KOSEN 1, ARICA