OBJECT N, 56858 (Decayed)
Orbit data source: Space-Track
OBJECT N, 56858 was a satellite in LEO that was launched on Wed, 07 Jun 2023 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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56858 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 N
1 56858U 23081N 25248.44781801 .11030718 24772-5 10008-2 0 9999
2 56858 97.2967 333.1874 0015267 265.3477 94.6078 16.38614757125941Epoch: 2025-09-05T10:44Z
TLE epoch observation values (Epoch: 2025-09-05T10:44:51.476Z)
Latitude
-0.00003°
Longitude
-172.82294°
Altitude
173.561 km
Speed
7.802 km/s
True Right ascension
22h 12m 44s
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
23:27:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
176.286 km
Perigee altitude
156.303 km
Semi-major axis
6,544.432 km
Eccentricity
0.00153
Inclination
97.2967°
RAAN
333.1874°
Arg. of periapsis
265.3477°
True anomaly
94.78215°
Mean anomaly
94.6078°
Eccentric anomaly
94.69498°
Mean motion
4.09954 °/min
Orbital period
87.81 mins
BSTAR
0.0010008
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Other satellites on launch #81 in the year 2023 (2023-06-07 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 N 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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