CZ-6A DEB, 55224 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 55224 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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55224 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: 8 months ago
TLE from 8 months ago
0 CZ-6A DEB
1 55224U 22151WR 25242.78906869 .05799080 41975-1 22345-1 0 9999
2 55224 98.6449 325.4304 0025717 300.6583 59.2151 15.90682024144300Epoch: 2025-08-30T18:56Z
TLE epoch observation values (Epoch: 2025-08-30T18:56:15.534Z)
Latitude
-0.00008°
Longitude
62.14736°
Altitude
294.759 km
Speed
7.736 km/s
True Right ascension
21h 41m 43s
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
23:39:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
314.472 km
Perigee altitude
280.137 km
Semi-major axis
6,675.442 km
Eccentricity
0.00257
Inclination
98.6449°
RAAN
325.4304°
Arg. of periapsis
300.6583°
True anomaly
59.46869°
Mean anomaly
59.2151°
Eccentric anomaly
59.34185°
Mean motion
3.97945 °/min
Orbital period
90.46 mins
BSTAR
0.022345
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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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