CZ-6A DEB, 55867 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 55867 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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55867 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: 2 months ago
TLE from 2 months ago
0 CZ-6A DEB
1 55867U 22151ZP 26139.19131979 .02852918 54134-2 12706-1 0 9994
2 55867 98.5970 226.2491 0027671 283.7138 76.1048 15.85001731175327Epoch: 2026-05-19T04:35Z
TLE epoch observation values (Epoch: 2026-05-19T04:35:30.029Z)
Latitude
-0.00008°
Longitude
-79.49478°
Altitude
315.059 km
Speed
7.722 km/s
True Right ascension
15h 04m 59s
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
17:04:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
331.772 km
Perigee altitude
294.74 km
Semi-major axis
6,691.393 km
Eccentricity
0.00277
Inclination
98.597°
RAAN
226.2491°
Arg. of periapsis
283.7138°
True anomaly
76.41286°
Mean anomaly
76.1048°
Eccentric anomaly
76.25881°
Mean motion
3.96523 °/min
Orbital period
90.79 mins
BSTAR
0.012706
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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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