OBJECT BB, 57327 (Decayed)
Orbit data source: Space-Track
OBJECT BB, 57327 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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57327 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 OBJECT BB
1 57327U 23091BB 25215.94783005 .07226389 25611-5 16265-2 0 9999
2 57327 97.5142 290.0171 0015369 258.0341 101.9230 16.29874339114825Epoch: 2025-08-03T22:44Z
TLE epoch observation values (Epoch: 2025-08-03T22:44:52.516Z)
Latitude
-0.00001°
Longitude
-3.96405°
Altitude
198.214 km
Speed
7.786 km/s
True Right ascension
19h 20m 04s
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
16:15:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
199.798 km
Perigee altitude
179.609 km
Semi-major axis
6,567.84 km
Eccentricity
0.00154
Inclination
97.5142°
RAAN
290.0171°
Arg. of periapsis
258.0341°
True anomaly
102.09525°
Mean anomaly
101.923°
Eccentric anomaly
102.00913°
Mean motion
4.07764 °/min
Orbital period
88.29 mins
BSTAR
0.0016265
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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 BB 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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