OBJECT AP, 57041 (Decayed)
Orbit data source: Space-Track
OBJECT AP, 57041 was a Chinese satellite in LEO that was launched on Thu, 15 Jun 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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57041 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 OBJECT AP
1 57041U 23085AP 25297.97598951 .16847760 26322-5 35170-3 0 9991
2 57041 97.4651 61.2428 0010396 265.5348 94.4767 16.46240703131944Epoch: 2025-10-24T23:25Z
TLE epoch observation values (Epoch: 2025-10-24T23:25:25.493Z)
Latitude
-0.00003°
Longitude
36.27341°
Altitude
153.048 km
Speed
7.814 km/s
True Right ascension
04h 04m 58s
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
21:30:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
152.839 km
Perigee altitude
139.274 km
Semi-major axis
6,524.193 km
Eccentricity
0.00104
Inclination
97.4651°
RAAN
61.2428°
Arg. of periapsis
265.5348°
True anomaly
94.59545°
Mean anomaly
94.4767°
Eccentric anomaly
94.53608°
Mean motion
4.11863 °/min
Orbital period
87.41 mins
BSTAR
0.0003517
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Other satellites on launch #85 in the year 2023 (2023-06-15 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 AP 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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