CZ-6A DEB, 54333 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54333 was space debris in SSO originally from a launch on Fri, 11 Nov 2022 UTC launched from the Taiyaun Space Center, China (TSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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54333 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 CZ-6A DEB
1 54333U 22151CC 26145.23084223 .04047539 23804-1 12578-1 0 9995
2 54333 98.6064 250.5828 0028684 277.0492 82.7518 15.95148766188901Epoch: 2026-05-25T05:32Z
TLE epoch observation values (Epoch: 2026-05-25T05:32:24.768Z)
Latitude
-0.00003°
Longitude
-75.342°
Altitude
288.694 km
Speed
7.736 km/s
True Right ascension
16h 42m 19s
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
21:48:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
303.936 km
Perigee altitude
265.711 km
Semi-major axis
6,662.961 km
Eccentricity
0.00287
Inclination
98.6064°
RAAN
250.5828°
Arg. of periapsis
277.0492°
True anomaly
83.07801°
Mean anomaly
82.7518°
Eccentric anomaly
82.91489°
Mean motion
3.99064 °/min
Orbital period
90.21 mins
BSTAR
0.012578
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Other satellites on launch #151 in the year 2022 (2022-11-11 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.CZ-6A DEB 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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