CZ-6A DEB, 58202
Orbit data source: Space-Track
CZ-6A DEB, 58202 is space debris in SSO originally from a launch on Tue, 31 Oct 2023 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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58202 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cone, 0.3 m
Radar Cross Section
0.159 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CZ-6A DEB
1 58202U 23168D 25308.80080499 .00024414 00000-0 11744-2 0 9997
2 58202 97.7944 328.6700 0002377 24.9410 335.1938 15.18783601110198Epoch: 2025-11-04T19:13Z
TLE epoch observation values (Epoch: 2025-11-04T19:13:09.551Z)
Latitude
0.00002°
Longitude
-3.90242°
Altitude
511.107 km
Speed
7.609 km/s
True Right ascension
21h 54m 40s
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
21:21:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.137 km
Perigee altitude
504.864 km
Semi-major axis
6,884.637 km
Eccentricity
0.00024
Inclination
97.7944°
RAAN
328.67°
Arg. of periapsis
24.941°
True anomaly
335.18237°
Mean anomaly
335.1938°
Eccentric anomaly
335.18808°
Mean motion
3.79946 °/min
Orbital period
94.75 mins
BSTAR
0.0011744
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Other satellites on launch #168 in the year 2023 (2023-10-31 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 forecast
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-05 01:39:41.343Z | 177.355° S | 2025-11-05 01:42:41.343Z | 220.553° SW | 39.945° | 2025-11-05 01:46:41.343Z | 340.649° N |
| 5 mins | 2025-11-05 14:45:41.343Z | 350.686° N | 2025-11-05 14:47:41.343Z | 304.826° NW | 33.29° | 2025-11-05 14:50:41.343Z | 220.712° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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