CZ-6A DEB, 54946 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54946 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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54946 intel report (Beta)
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Edit Public Description
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: 2 months ago
TLE from 2 months ago
0 CZ-6A DEB
1 54946U 22151SK 25279.25742673 .04837666 00000-0 23618-1 0 9991
2 54946 98.9876 35.8199 0032767 326.5417 33.3773 15.77817241 82598Epoch: 2025-10-06T06:10Z
TLE epoch observation values (Epoch: 2025-10-06T06:10:41.669Z)
Latitude
-0.00007°
Longitude
-72.01698°
Altitude
321.388 km
Speed
7.726 km/s
True Right ascension
02h 23m 16s
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
15:08:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
355.584 km
Perigee altitude
311.6 km
Semi-major axis
6,711.729 km
Eccentricity
0.00328
Inclination
98.9876°
RAAN
35.8199°
Arg. of periapsis
326.5417°
True anomaly
33.58458°
Mean anomaly
33.3773°
Eccentric anomaly
33.48087°
Mean motion
3.94722 °/min
Orbital period
91.2 mins
BSTAR
0.023618
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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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