CZ-6A DEB, 54334 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54334 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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54334 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, 0.050 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 54334U 22151CD 26268.71472362 .07720991 20421+0 15308-1 0 9997
2 54334 98.5912 25.4686 0019117 302.6874 57.2560 16.07316012207309Epoch: 2026-09-25T17:09Z
TLE epoch observation values (Epoch: 2026-09-25T17:09:12.120Z)
Latitude
-0.00006°
Longitude
123.63494°
Altitude
250.544 km
Speed
7.761 km/s
True Right ascension
01h 41m 52s
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
04:53:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
263.797 km
Perigee altitude
238.45 km
Semi-major axis
6,629.261 km
Eccentricity
0.00191
Inclination
98.5912°
RAAN
25.4686°
Arg. of periapsis
302.6874°
True anomaly
57.44049°
Mean anomaly
57.256°
Eccentric anomaly
57.34822°
Mean motion
4.02111 °/min
Orbital period
89.53 mins
BSTAR
0.015308
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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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