OBJECT F, 55253 (Decayed)
Orbit data source: Space-Track
OBJECT F, 55253 was a Chinese satellite in LEO that was launched on Sun, 15 Jan 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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55253 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT F
1 55253U 23007F 25054.68724622 .08692571 41166-3 80887-3 0 9998
2 55253 97.2572 137.0352 0009818 275.0688 84.9490 16.38691279118294Epoch: 2025-02-23T16:29Z
TLE epoch observation values (Epoch: 2025-02-23T16:29:38.073Z)
Latitude
-0.00006°
Longitude
95.81031°
Altitude
171.98 km
Speed
7.803 km/s
True Right ascension
09h 08m 08s
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
23:19:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
172.514 km
Perigee altitude
159.664 km
Semi-major axis
6,544.226 km
Eccentricity
0.00098
Inclination
97.2572°
RAAN
137.0352°
Arg. of periapsis
275.0688°
True anomaly
85.06108°
Mean anomaly
84.949°
Eccentric anomaly
85.00504°
Mean motion
4.09973 °/min
Orbital period
87.81 mins
BSTAR
0.00080887
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Other satellites on launch #7 in the year 2023 (2023-01-15 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 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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