OBJECT BA, 57326 (Decayed)
Orbit data source: Space-Track
OBJECT BA, 57326 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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57326 intel report (Beta)
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Identifier
Orbit
Country
TBDRelated business
OOO Stratonavtika (RU)Manufacturer
MKS
Mission
Decayed Commercial Communications
Bus & Motor
TINYSAT 2TU, Unknown motor
Mass
0.25 kg wet, 0.25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.006 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 OBJECT BA
1 57326U 23091BA 26157.85242748 .08018696 25705-5 11040-2 0 9999
2 57326 97.4819 241.4388 0014408 270.1398 89.8248 16.34882943161780Epoch: 2026-06-06T20:27Z
TLE epoch observation values (Epoch: 2026-06-06T20:27:29.734Z)
Latitude
0.00005°
Longitude
39.30286°
Altitude
182.677 km
Speed
7.797 km/s
True Right ascension
16h 05m 45s
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
14:27:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
185.712 km
Perigee altitude
166.824 km
Semi-major axis
6,554.405 km
Eccentricity
0.00144
Inclination
97.4819°
RAAN
241.4388°
Arg. of periapsis
270.1398°
True anomaly
89.9899°
Mean anomaly
89.8248°
Eccentric anomaly
89.90735°
Mean motion
4.09019 °/min
Orbital period
88.02 mins
BSTAR
0.001104
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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 BA 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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