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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
20 hours 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 (3 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 20 hours ago
0 TEIKYOSAT-4 (OORURI)
1 49396U 21102B   25118.66859940  .00003855  00000-0  25812-3 0  9993
2 49396  97.4129 158.6053 0011016 277.9561  82.0417 15.07436782190239
Epoch: 2025-04-28T16:02Z
Definitive object data (Epoch: 2025-04-28T16:02:46.988Z)
Latitude
-0°
Longitude
61.0302°
Altitude
546.061 km
Speed
7.59 km/s
True Right ascension
10h 34m 25s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
38.93264°
Longitude
-112.17706°
Altitude
554.895 km
Speed
7.585 km/s
Apparent Right ascension
02h 48m 38s
Apparent Declination
3° 06' 56"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
19:17:30
Azimuth
72.525° E
Elevation
-15.172°
Doppler factor
1
Orbital elements
Apogee altitude
548.641 km
Perigee altitude
533.397 km
Semi-major axis
6,919.156 km
Eccentricity
0.0011016
Inclination
97.4129°
RAAN
158.6053°
Arg. of periapsis
277.9561°
True anomaly
82.16674°
Mean anomaly
82.0417°
Eccentric anomaly
82.10422°
Mean motion
3.77106 °/min
BSTAR
0.00025812
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.
6 mins2025-04-29 14:55:13.294Z34.46° NE2025-04-29 14:58:13.294Z91.08° ESE28.517°2025-04-29 15:01:13.294Z156.82° SSE
4 mins2025-04-29 16:31:13.294Z320.203° NNW2025-04-29 16:33:13.294Z283.647° WNW16.208°2025-04-29 16:35:13.294Z252.485° W
4 mins2025-04-30 01:40:13.294Z94.335° ESE2025-04-30 01:41:13.294Z76.882° E16.124°2025-04-30 01:44:13.294Z26.925° NE
5 mins2025-04-30 03:14:13.294Z214.936° SW2025-04-30 03:16:13.294Z267.982° W28.565°2025-04-30 03:19:13.294Z325.363° NNW
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