OBJECT A, 51824 (Decayed)
Orbit data source: Space-Track
OBJECT A, 51824 was a Chinese satellite in LEO that was launched on Sun, 27 Feb 2022 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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51824 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 OBJECT A
1 51824U 22019A 26001.67406597 .13547712 25473-5 24614-3 0 9993
2 51824 97.3609 98.1254 0009626 276.2967 83.7240 16.47108187214450Epoch: 2026-01-01T16:10Z
TLE epoch observation values (Epoch: 2026-01-01T16:10:39.299Z)
Latitude
-0.00002°
Longitude
114.13641°
Altitude
149.543 km
Speed
7.817 km/s
True Right ascension
06h 32m 30s
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
16:04:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
150.036 km
Perigee altitude
137.48 km
Semi-major axis
6,521.895 km
Eccentricity
0.00096
Inclination
97.3609°
RAAN
98.1254°
Arg. of periapsis
276.2967°
True anomaly
83.83366°
Mean anomaly
83.724°
Eccentric anomaly
83.77883°
Mean motion
4.12081 °/min
Orbital period
87.36 mins
BSTAR
0.00024614
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Other satellites on launch #19 in the year 2022 (2022-02-27 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 A 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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