CZ-6A DEB, 56631 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 56631 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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56631 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: 2 months ago
TLE from 2 months ago
0 CZ-6A DEB
1 56631U 22151AFF 26199.24680129 .00385479 00000-0 50443-2 0 9995
2 56631 98.5992 298.7980 0005397 225.8856 134.1952 15.57278960173408Epoch: 2026-07-18T05:55Z
TLE epoch observation values (Epoch: 2026-07-18T05:55:23.631Z)
Latitude
-0.00003°
Longitude
-86.11275°
Altitude
401.189 km
Speed
7.668 km/s
True Right ascension
19h 55m 11s
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
06:01:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
396.162 km
Perigee altitude
388.854 km
Semi-major axis
6,770.645 km
Eccentricity
0.00054
Inclination
98.5992°
RAAN
298.798°
Arg. of periapsis
225.8856°
True anomaly
134.23952°
Mean anomaly
134.1952°
Eccentric anomaly
134.21736°
Mean motion
3.89581 °/min
Orbital period
92.41 mins
BSTAR
0.0050443
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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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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