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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 (4 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: 12 hours ago

TLE from 12 hours ago
0 TEIKYOSAT-4 (OORURI)
1 49396U 21102B   26095.06401827  .00002476  00000-0  15918-3 0  9993
2 49396  97.3747 127.3760 0012149 176.7358 183.3953 15.09248638241690
Epoch: 2026-04-05T01:32Z
TLE epoch observation values (Epoch: 2026-04-05T01:32:11.178Z)
Latitude
-0.00001°
Longitude
-89.04538°
Altitude
549.961 km
Speed
7.582 km/s
True Right ascension
08h 29m 30s
True Declination
0° 00' 00"
Sunlit
Object was in partial shadow 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
19:17:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.873 km
Perigee altitude
527.074 km
Semi-major axis
6,913.61 km
Eccentricity
0.00121
Inclination
97.3747°
RAAN
127.376°
Arg. of periapsis
176.7358°
True anomaly
183.38707°
Mean anomaly
183.3953°
Eccentric anomaly
183.39118°
Mean motion
3.7756 °/min
Orbital period
95.35 mins
BSTAR
0.00015918
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