OBJECT AQ, 57042 (Decayed)
Orbit data source: Space-Track
OBJECT AQ, 57042 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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57042 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 AQ
1 57042U 23085AQ 25280.48228669 .15235839 26321-5 23836-3 0 9998
2 57042 97.4492 43.1983 0010048 265.2659 94.7497 16.47933047129287Epoch: 2025-10-07T11:34Z
TLE epoch observation values (Epoch: 2025-10-07T11:34:29.570Z)
Latitude
-0.00006°
Longitude
-146.79545°
Altitude
148.594 km
Speed
7.817 km/s
True Right ascension
02h 52m 47s
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
21:32:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
148.135 km
Perigee altitude
135.033 km
Semi-major axis
6,519.721 km
Eccentricity
0.001
Inclination
97.4492°
RAAN
43.1983°
Arg. of periapsis
265.2659°
True anomaly
94.86443°
Mean anomaly
94.7497°
Eccentric anomaly
94.80707°
Mean motion
4.12287 °/min
Orbital period
87.32 mins
BSTAR
0.00023836
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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 AQ 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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