CZ-6A DEB, 54987 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54987 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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54987 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 54987U 22151UC 26007.98216253 .01456355 00000-0 71817-2 0 9990
2 54987 99.0426 173.2844 0027422 317.1958 42.7168 15.78980182 97165Epoch: 2026-01-07T23:34Z
TLE epoch observation values (Epoch: 2026-01-07T23:34:18.842Z)
Latitude
-0.00005°
Longitude
72.16309°
Altitude
322.944 km
Speed
7.722 km/s
True Right ascension
11h 33m 08s
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
23:38:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
348.692 km
Perigee altitude
311.9 km
Semi-major axis
6,708.433 km
Eccentricity
0.00274
Inclination
99.0426°
RAAN
173.2844°
Arg. of periapsis
317.1958°
True anomaly
42.93051°
Mean anomaly
42.7168°
Eccentric anomaly
42.8236°
Mean motion
3.95013 °/min
Orbital period
91.14 mins
BSTAR
0.0071817
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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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