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TEIKYOSAT-4 (OORURI), 49396

Orbit data source: Space-Track

TEIKYOSAT-4 (OORURI), 49396 is a payload satellite owned by Teikyo (JP) in SSO that was launched on Tue, 09 Nov 2021 UTC via an EPSILON launch vehicle from the Kagoshima Space Center University Of Tokyo (KSCUT). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
49396, 2021-102B
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
Teikyo
Mission
Operational Amateur Technology
Bus & Motor
TEIKYOSAT, Unknown motor
Mass
52 kg wet, 52 kg dry
Launch date (UTC)
2021-11-09 (5 years ago)
Launch vehicle
EPSILON
Launch site
Kagoshima Space Center University Of Tokyo (KSCUT)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.454 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 TEIKYOSAT-4 (OORURI)
1 49396U 21102B   26155.06159113  .00001860  00000-0  11983-3 0  9992
2 49396  97.3671 185.0554 0011461 346.7674  13.3253 15.09460709250740
Epoch: 2026-06-04T01:28Z
TLE epoch observation values (Epoch: 2026-06-04T01:28:41.473Z)
Latitude
-0.00005°
Longitude
-89.62866°
Altitude
533.21 km
Speed
7.6 km/s
True Right ascension
12h 20m 13s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
12:28:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
542.748 km
Perigee altitude
526.902 km
Semi-major axis
6,912.962 km
Eccentricity
0.00115
Inclination
97.3671°
RAAN
185.0554°
Arg. of periapsis
346.7674°
True anomaly
13.35561°
Mean anomaly
13.3253°
Eccentric anomaly
13.34045°
Mean motion
3.77613 °/min
Orbital period
95.34 mins
BSTAR
0.00011983
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