CZ-6A DEB, 55885 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 55885 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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55885 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: 9 months ago
TLE from 9 months ago
0 CZ-6A DEB
1 55885U 22151AAH 25092.10760857 .02086384 00000-0 26615-1 0 9996
2 55885 98.5867 144.1619 0015872 203.8363 156.2155 15.56062658 47943Epoch: 2025-04-02T02:34Z
TLE epoch observation values (Epoch: 2025-04-02T02:34:57.380Z)
Latitude
0.00001°
Longitude
-85.27673°
Altitude
412.016 km
Speed
7.658 km/s
True Right ascension
09h 36m 38s
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
14:52:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
406.791 km
Perigee altitude
385.287 km
Semi-major axis
6,774.176 km
Eccentricity
0.00159
Inclination
98.5867°
RAAN
144.1619°
Arg. of periapsis
203.8363°
True anomaly
156.28872°
Mean anomaly
156.2155°
Eccentric anomaly
156.25212°
Mean motion
3.89277 °/min
Orbital period
92.48 mins
BSTAR
0.026615
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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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