CZ-6A DEB, 55881 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 55881 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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55881 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: 4 months ago
TLE from 4 months ago
0 CZ-6A DEB
1 55881U 22151AAD 26008.18720217 .00772989 00000-0 10549-1 0 9994
2 55881 98.6462 97.9081 0025471 318.9203 41.0128 15.54542543156324Epoch: 2026-01-08T04:29Z
TLE epoch observation values (Epoch: 2026-01-08T04:29:34.267Z)
Latitude
-0.00006°
Longitude
-77.22958°
Altitude
393.563 km
Speed
7.681 km/s
True Right ascension
06h 31m 37s
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
09:54:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
417.727 km
Perigee altitude
383.195 km
Semi-major axis
6,778.598 km
Eccentricity
0.00255
Inclination
98.6462°
RAAN
97.9081°
Arg. of periapsis
318.9203°
True anomaly
41.2048°
Mean anomaly
41.0128°
Eccentric anomaly
41.10875°
Mean motion
3.88896 °/min
Orbital period
92.57 mins
BSTAR
0.010549
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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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