CZ-6A DEB, 54947 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 54947 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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54947 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, 0.050 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 CZ-6A DEB
1 54947U 22151SL 26258.05636016 .03146072 11176-1 86106-2 0 9993
2 54947 99.0752 105.9831 0010651 270.6617 89.3433 15.96752999206338Epoch: 2026-09-15T01:21Z
TLE epoch observation values (Epoch: 2026-09-15T01:21:09.517Z)
Latitude
-0.0001°
Longitude
91.66568°
Altitude
286.499 km
Speed
7.736 km/s
True Right ascension
07h 03m 55s
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
04:53:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
287.473 km
Perigee altitude
273.289 km
Semi-major axis
6,658.518 km
Eccentricity
0.00107
Inclination
99.0752°
RAAN
105.9831°
Arg. of periapsis
270.6617°
True anomaly
89.46535°
Mean anomaly
89.3433°
Eccentric anomaly
89.40432°
Mean motion
3.99463 °/min
Orbital period
90.12 mins
BSTAR
0.0086106
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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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