CZ-6A DEB, 54578 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54578 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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54578 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 54578U 22151ME 26135.19224742 .03965204 19805-1 12227-1 0 9996
2 54578 98.5762 227.5177 0028749 285.8709 73.9394 15.94562099115426Epoch: 2026-05-15T04:36Z
TLE epoch observation values (Epoch: 2026-05-15T04:36:50.177Z)
Latitude
-0.00002°
Longitude
-74.61846°
Altitude
287.435 km
Speed
7.738 km/s
True Right ascension
15h 10m 04s
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
21:35:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
305.618 km
Perigee altitude
267.298 km
Semi-major axis
6,664.595 km
Eccentricity
0.00287
Inclination
98.5762°
RAAN
227.5177°
Arg. of periapsis
285.8709°
True anomaly
74.25629°
Mean anomaly
73.9394°
Eccentric anomaly
74.09782°
Mean motion
3.98917 °/min
Orbital period
90.24 mins
BSTAR
0.012227
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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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