DECAYED

OBJECT AA, 57190 (Decayed)

Orbit data source: Space-Track

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Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT AA, 57190 was a satellite in LEO that was launched on Tue, 27 Jun 2023 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
Identifier
57190, 2023-091AA
Orbit
Decayed
Country
Flag of TBDTBD
Related business
Flag of RUOrel State University (RU)
Manufacturer
Sputniks
Mission
Decayed Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
2.2 kg wet, 2.2 kg dry
Launch date (UTC)
2023-06-27 (3 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Vostochny Cosmodrome (VOSTO)
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 2 months ago

TLE from 2 months ago
0 OBJECT AA
1 57190U 23091AA  26110.07929209  .10484263  25974-5  74814-3 0  9992
2 57190  97.4781 194.6613 0013966 266.7755  93.1946 16.39851341156851
Epoch: 2026-04-20T01:54Z
TLE epoch observation values (Epoch: 2026-04-20T01:54:10.836Z)
Latitude
-0.00006°
Longitude
-42.05842°
Altitude
169.969 km
Speed
7.804 km/s
True Right ascension
12h 58m 38s
True Declination
0° 00' 00"
Sunlit
Object was in full 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
18:38:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
172.145 km
Perigee altitude
153.874 km
Semi-major axis
6,541.146 km
Eccentricity
0.0014
Inclination
97.4781°
RAAN
194.6613°
Arg. of periapsis
266.7755°
True anomaly
93.35437°
Mean anomaly
93.1946°
Eccentric anomaly
93.27449°
Mean motion
4.10263 °/min
Orbital period
87.75 mins
BSTAR
0.00074814
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