CZ-6A DEB, 54328 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54328 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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54328 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 CZ-6A DEB
1 54328U 22151BX 26219.90065691 .04683968 44863-1 64699-2 0 9995
2 54328 98.6094 347.4010 0028297 289.5845 70.2379 16.09457550128863Epoch: 2026-08-07T21:36Z
TLE epoch observation values (Epoch: 2026-08-07T21:36:56.757Z)
Latitude
-0.00008°
Longitude
66.74481°
Altitude
245.209 km
Speed
7.763 km/s
True Right ascension
23h 09m 36s
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
07:00:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
263.979 km
Perigee altitude
226.495 km
Semi-major axis
6,623.374 km
Eccentricity
0.00283
Inclination
98.6094°
RAAN
347.401°
Arg. of periapsis
289.5845°
True anomaly
70.54343°
Mean anomaly
70.2379°
Eccentric anomaly
70.39063°
Mean motion
4.02647 °/min
Orbital period
89.41 mins
BSTAR
0.0064699
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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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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