OBJECT AH, 57035 (Decayed)
Orbit data source: Space-Track
OBJECT AH, 57035 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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57035 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 AH
1 57035U 23085AH 25284.23154418 .18389639 26343-5 34032-3 0 9992
2 57035 97.4509 47.0059 0009542 264.0190 96.0025 16.47011739129859Epoch: 2025-10-11T05:33Z
TLE epoch observation values (Epoch: 2025-10-11T05:33:25.417Z)
Latitude
-0.00006°
Longitude
-56.41599°
Altitude
151.133 km
Speed
7.815 km/s
True Right ascension
03h 08m 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
21:31:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
150.241 km
Perigee altitude
137.794 km
Semi-major axis
6,522.154 km
Eccentricity
0.00095
Inclination
97.4509°
RAAN
47.0059°
Arg. of periapsis
264.019°
True anomaly
96.11123°
Mean anomaly
96.0025°
Eccentric anomaly
96.05687°
Mean motion
4.12056 °/min
Orbital period
87.37 mins
BSTAR
0.00034032
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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 AH 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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