OBJECT F, 58825 (Decayed)
Orbit data source: Space-Track
OBJECT F, 58825 was a Chinese satellite in LEO that was launched on Tue, 23 Jan 2024 UTC via a LIJIAN-1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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58825 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 OBJECT F
1 58825U 24016F 25320.85257990 .17035075 26217-5 86603-3 0 9995
2 58825 97.4436 52.7321 0010359 252.5709 107.4459 16.41836546101669Epoch: 2025-11-16T20:27Z
TLE epoch observation values (Epoch: 2025-11-16T20:27:42.903Z)
Latitude
-0.00002°
Longitude
49.64192°
Altitude
166.212 km
Speed
7.805 km/s
True Right ascension
03h 30m 55s
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
21:29:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
164.499 km
Perigee altitude
150.958 km
Semi-major axis
6,535.866 km
Eccentricity
0.00104
Inclination
97.4436°
RAAN
52.7321°
Arg. of periapsis
252.5709°
True anomaly
107.5591°
Mean anomaly
107.4459°
Eccentric anomaly
107.5025°
Mean motion
4.1076 °/min
Orbital period
87.64 mins
BSTAR
0.00086603
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Other satellites on launch #16 in the year 2024 (2024-01-23 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 F 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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