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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
Last TLE update
1 day ago
Origin
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, 0.55 m
Radar Cross Section
0.454 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 1 day ago
0 TEIKYOSAT-4 (OORURI)
1 49396U 21102B   25132.67427538  .00001942  00000-0  13170-3 0  9993
2 49396  97.4116 172.1088 0011435 223.6581 136.3744 15.07518756192341
Epoch: 2025-05-12T16:10Z
Definitive object data (Epoch: 2025-05-12T16:10:57.392Z)
Latitude
-0.00001°
Longitude
58.6857°
Altitude
552.593 km
Speed
7.582 km/s
True Right ascension
11h 28m 26s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
-64.35584°
Longitude
75.39526°
Altitude
566.303 km
Speed
7.578 km/s
Apparent Right ascension
14h 21m 22s
Apparent Declination
-54° 18' 17"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
03:25:09
Azimuth
148.631° SSE
Elevation
-72.067°
Doppler factor
1
Orbital elements
Apogee altitude
548.679 km
Perigee altitude
532.856 km
Semi-major axis
6,918.905 km
Eccentricity
0.0011435
Inclination
97.4116°
RAAN
172.1088°
Arg. of periapsis
223.6581°
True anomaly
136.46471°
Mean anomaly
136.3744°
Eccentric anomaly
136.41957°
Mean motion
3.77127 °/min
BSTAR
0.0001317
Orbital period
95.46 mins
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TEIKYOSAT-4 (OORURI) Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
5 mins2025-05-14 01:47:29.592Z109.334° ESE2025-05-14 01:49:29.592Z71.944° E20.139°2025-05-14 01:52:29.592Z20.216° NNE
4 mins2025-05-14 03:22:29.592Z227.392° WSW2025-05-14 03:24:29.592Z274.724° WNW23.303°2025-05-14 03:26:29.592Z312.776° NW
5 mins2025-05-14 14:58:29.592Z49.349° ENE2025-05-14 15:00:29.592Z108.447° ESE29.924°2025-05-14 15:03:29.592Z163.438° S
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