OBJECT AW, 57322 (Decayed)
Orbit data source: Space-Track
OBJECT AW, 57322 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.
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57322 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
OOO Stratonavtika (RU)Manufacturer
MKS
Mission
Decayed Commercial Communications
Bus & Motor
TINYSAT 1TU, Unknown motor
Mass
0.125 kg wet, 0.125 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.0 m
Radar Cross Section
0.004 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 OBJECT AW
1 57322U 23091AW 25215.67503098 .07408063 25679-5 15142-2 0 9994
2 57322 97.5141 289.6996 0015448 266.2521 93.7007 16.30886971114947Epoch: 2025-08-03T16:12Z
TLE epoch observation values (Epoch: 2025-08-03T16:12:02.676Z)
Latitude
-0.00002°
Longitude
94.195°
Altitude
194.064 km
Speed
7.789 km/s
True Right ascension
19h 18m 47s
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
05:21:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
197.124 km
Perigee altitude
176.84 km
Semi-major axis
6,565.119 km
Eccentricity
0.00154
Inclination
97.5141°
RAAN
289.6996°
Arg. of periapsis
266.2521°
True anomaly
93.87733°
Mean anomaly
93.7007°
Eccentric anomaly
93.78902°
Mean motion
4.08018 °/min
Orbital period
88.23 mins
BSTAR
0.0015142
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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 AW Visibility
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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. |
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| This satellite is decayed. |
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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