CZ-6A DEB, 54975 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54975 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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54975 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: 3 weeks ago
TLE from 3 weeks ago
0 CZ-6A DEB
1 54975U 22151TQ 26154.33454806 .02512455 38294-2 10204-1 0 9992
2 54975 98.8145 295.4809 0028127 269.8476 89.9568 15.86493467190374Epoch: 2026-06-03T08:01Z
TLE epoch observation values (Epoch: 2026-06-03T08:01:44.952Z)
Latitude
0.00005°
Longitude
-76.75106°
Altitude
315.296 km
Speed
7.719 km/s
True Right ascension
19h 41m 55s
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
23:07:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
327.877 km
Perigee altitude
290.259 km
Semi-major axis
6,687.205 km
Eccentricity
0.00281
Inclination
98.8145°
RAAN
295.4809°
Arg. of periapsis
269.8476°
True anomaly
90.27911°
Mean anomaly
89.9568°
Eccentric anomaly
90.11796°
Mean motion
3.96896 °/min
Orbital period
90.7 mins
BSTAR
0.010204
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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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