CZ-6A DEB, 54359 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54359 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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54359 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 week ago
TLE from 1 week ago
0 CZ-6A DEB
1 54359U 22151DE 26120.40638180 .03934498 23075-1 10894-1 0 9999
2 54359 98.9890 283.6974 0025542 311.6843 48.2243 15.97387935113672Epoch: 2026-04-30T09:45Z
TLE epoch observation values (Epoch: 2026-04-30T09:45:11.387Z)
Latitude
0.00002°
Longitude
-80.95349°
Altitude
273.501 km
Speed
7.75 km/s
True Right ascension
18h 54m 47s
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
22:58:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
295.612 km
Perigee altitude
261.607 km
Semi-major axis
6,656.747 km
Eccentricity
0.00255
Inclination
98.989°
RAAN
283.6974°
Arg. of periapsis
311.6843°
True anomaly
48.44304°
Mean anomaly
48.2243°
Eccentric anomaly
48.33362°
Mean motion
3.99623 °/min
Orbital period
90.08 mins
BSTAR
0.010894
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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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