OBJECT AN, 57202
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 AN, 57202 is a satellite in SSO 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.
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57202 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
TBDRelated business
OOO Special Technological Center (RU)Manufacturer
STTS/SPBPU
Mission
Operational Commercial Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
3 kg wet, 3 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT AN
1 57202U 23091AN 25304.31143410 .00009561 00000-0 49813-3 0 9991
2 57202 97.5470 359.3972 0010103 176.2281 183.9029 15.16162205129249Epoch: 2025-10-31T07:28Z
TLE epoch observation values (Epoch: 2025-10-31T07:28:27.906Z)
Latitude
-0.00007°
Longitude
-152.57675°
Altitude
527.486 km
Speed
7.595 km/s
True Right ascension
23h 57m 35s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:31:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.393 km
Perigee altitude
507.466 km
Semi-major axis
6,892.566 km
Eccentricity
0.00101
Inclination
97.547°
RAAN
359.3972°
Arg. of periapsis
176.2281°
True anomaly
183.89503°
Mean anomaly
183.9029°
Eccentric anomaly
183.89896°
Mean motion
3.7929 °/min
Orbital period
94.91 mins
BSTAR
0.00049813
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Other satellites on launch #91 in the year 2023 (2023-06-27 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT AN Visibility forecast
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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 mins | 2025-10-31 15:58:16.744Z | 45.087° ENE | 2025-10-31 16:01:16.744Z | 107.078° ESE | 21.802° | 2025-10-31 16:03:16.744Z | 144.887° SSE |
| 4 mins | 2025-10-31 17:33:16.744Z | 322.702° NNW | 2025-10-31 17:35:16.744Z | 279.841° WNW | 18.749° | 2025-10-31 17:37:16.744Z | 245.556° WSW |
| 5 mins | 2025-11-01 04:12:16.744Z | 196.876° SSW | 2025-11-01 04:14:16.744Z | 255.705° W | 35.849° | 2025-11-01 04:17:16.744Z | 331.487° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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