OBJECT S, 57020 (Decayed)
Orbit data source: Space-Track
OBJECT S, 57020 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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57020 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 OBJECT S
1 57020U 23085S 25272.89447634 .18501208 26030-5 37470-3 0 9990
2 57020 97.4534 36.4948 0009767 274.5234 85.4953 16.46480378128134Epoch: 2025-09-29T21:28Z
TLE epoch observation values (Epoch: 2025-09-29T21:28:02.755Z)
Latitude
-0.00003°
Longitude
65.59168°
Altitude
151.384 km
Speed
7.816 km/s
True Right ascension
02h 25m 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
21:31:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
151.794 km
Perigee altitude
139.05 km
Semi-major axis
6,523.559 km
Eccentricity
0.00098
Inclination
97.4534°
RAAN
36.4948°
Arg. of periapsis
274.5234°
True anomaly
85.60689°
Mean anomaly
85.4953°
Eccentric anomaly
85.55109°
Mean motion
4.11923 °/min
Orbital period
87.39 mins
BSTAR
0.0003747
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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 S 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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