OBJECT B, 53300 (Decayed)
Orbit data source: Space-Track
OBJECT B, 53300 was a satellite owned by CAS (CN) in LEO that was launched on Wed, 27 Jul 2022 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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53300 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Decayed Civil Technology
Bus & Motor
Unknown
Mass
94 kg wet, 94 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT B
1 53300U 22087B 25104.32862511 .06252011 24491-5 67966-3 0 9999
2 53300 97.2632 196.6640 0012250 264.5273 95.4628 16.37190370152541Epoch: 2025-04-14T07:53Z
TLE epoch observation values (Epoch: 2025-04-14T07:53:13.209Z)
Latitude
-0.00003°
Longitude
-124.38619°
Altitude
177.313 km
Speed
7.799 km/s
True Right ascension
13h 06m 39s
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
21:25:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
178.114 km
Perigee altitude
162.071 km
Semi-major axis
6,548.229 km
Eccentricity
0.00123
Inclination
97.2632°
RAAN
196.664°
Arg. of periapsis
264.5273°
True anomaly
95.60252°
Mean anomaly
95.4628°
Eccentric anomaly
95.53266°
Mean motion
4.09598 °/min
Orbital period
87.89 mins
BSTAR
0.00067966
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Other satellites on launch #87 in the year 2022 (2022-07-27 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 B 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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