OBJECT B, 57425 (Decayed)
Orbit data source: Space-Track
OBJECT B, 57425 was a Chinese satellite in LEO that was launched on Sun, 23 Jul 2023 UTC via a CHANG ZHENG 2D launch vehicle from the Taiyaun Space Center, China (TSC). 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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57425 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 OBJECT B
1 57425U 23104B 26087.82909689 .09696374 24827-5 29503-3 0 9991
2 57425 97.2606 178.5517 0014627 269.1524 90.8102 16.43696874151155Epoch: 2026-03-28T19:53Z
TLE epoch observation values (Epoch: 2026-03-28T19:53:53.971Z)
Latitude
0.00001°
Longitude
53.83309°
Altitude
159.396 km
Speed
7.81 km/s
True Right ascension
11h 54m 12s
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
22:27:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
162.336 km
Perigee altitude
143.231 km
Semi-major axis
6,530.92 km
Eccentricity
0.00146
Inclination
97.2606°
RAAN
178.5517°
Arg. of periapsis
269.1524°
True anomaly
90.97779°
Mean anomaly
90.8102°
Eccentric anomaly
90.894°
Mean motion
4.11227 °/min
Orbital period
87.54 mins
BSTAR
0.00029503
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Other satellites on launch #104 in the year 2023 (2023-07-23 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 B 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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