CZ-6A DEB, 55202 (Decayed)
Orbit data source: Space-Track
CZ-6A DEB, 55202 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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55202 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 55202U 22151VT 26174.52779086 .04777474 35388-1 14903-1 0 9995
2 55202 98.5765 268.9096 0025606 279.5142 80.3237 15.95568736188000Epoch: 2026-06-23T12:40Z
TLE epoch observation values (Epoch: 2026-06-23T12:40:01.130Z)
Latitude
0.00005°
Longitude
167.20681°
Altitude
287.058 km
Speed
7.737 km/s
True Right ascension
17h 55m 38s
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
03:52:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
300.71 km
Perigee altitude
266.594 km
Semi-major axis
6,661.789 km
Eccentricity
0.00256
Inclination
98.5765°
RAAN
268.9096°
Arg. of periapsis
279.5142°
True anomaly
80.6131°
Mean anomaly
80.3237°
Eccentric anomaly
80.46839°
Mean motion
3.99169 °/min
Orbital period
90.19 mins
BSTAR
0.014903
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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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