CZ-6A DEB, 54582 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54582 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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54582 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: 6 months ago
TLE from 6 months ago
0 CZ-6A DEB
1 54582U 22151MJ 25364.68852330 .08195132 20270+0 19583-1 0 9996
2 54582 98.5894 92.4622 0019889 325.2620 34.7356 16.03798275167335Epoch: 2025-12-30T16:31Z
TLE epoch observation values (Epoch: 2025-12-30T16:31:28.413Z)
Latitude
-0.00004°
Longitude
105.22561°
Altitude
256.226 km
Speed
7.76 km/s
True Right ascension
06h 09m 50s
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
21:35:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
274.027 km
Perigee altitude
247.618 km
Semi-major axis
6,638.96 km
Eccentricity
0.00199
Inclination
98.5894°
RAAN
92.4622°
Arg. of periapsis
325.262°
True anomaly
34.86573°
Mean anomaly
34.7356°
Eccentric anomaly
34.80064°
Mean motion
4.0123 °/min
Orbital period
89.72 mins
BSTAR
0.019583
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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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