OBJECT AE, 57032 (Decayed)
Orbit data source: Space-Track
OBJECT AE, 57032 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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57032 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 AE
1 57032U 23085AE 25281.74536939 .16146852 26103-5 38592-3 0 9999
2 57032 97.4531 45.0045 0014688 272.8751 87.0869 16.44969779129478Epoch: 2025-10-08T17:53Z
TLE epoch observation values (Epoch: 2025-10-08T17:53:19.915Z)
Latitude
-0.0001°
Longitude
119.05603°
Altitude
155.398 km
Speed
7.813 km/s
True Right ascension
03h 00m 01s
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
21:31:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
159.007 km
Perigee altitude
139.831 km
Semi-major axis
6,527.556 km
Eccentricity
0.00147
Inclination
97.4531°
RAAN
45.0045°
Arg. of periapsis
272.8751°
True anomaly
87.25501°
Mean anomaly
87.0869°
Eccentric anomaly
87.17095°
Mean motion
4.11545 °/min
Orbital period
87.48 mins
BSTAR
0.00038592
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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 AE 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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