CZ-6A DEB, 63392
Orbit data source: Space-Track
CZ-6A DEB, 63392 is space debris in LEO originally from a launch on Tue, 06 Aug 2024 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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63392 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
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: 18 hours ago
TLE from 18 hours ago
0 CZ-6A DEB
1 63392U 24140ADP 26116.88708721 .00000357 00000-0 15694-3 0 9994
2 63392 89.0276 282.7343 0036913 353.9530 6.1210 14.21155436 86664Epoch: 2026-04-26T21:17Z
TLE epoch observation values (Epoch: 2026-04-26T21:17:24.334Z)
Latitude
-0.00003°
Longitude
108.49825°
Altitude
798.074 km
Speed
7.468 km/s
True Right ascension
18h 50m 56s
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
22:58:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
844.962 km
Perigee altitude
791.833 km
Semi-major axis
7,196.534 km
Eccentricity
0.00369
Inclination
89.0276°
RAAN
282.7343°
Arg. of periapsis
353.953°
True anomaly
6.16631°
Mean anomaly
6.121°
Eccentric anomaly
6.14363°
Mean motion
3.55515 °/min
Orbital period
101.26 mins
BSTAR
0.00015694
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Other satellites on launch #140 in the year 2024 (2024-08-06 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-04-27 23:12:29.082Z | 3.559° NNE | 2026-04-27 23:17:29.082Z | 66.211° ENE | 44.456° | 2026-04-27 23:22:29.082Z | 177.657° S |
| 7 mins | 2026-04-28 10:36:29.082Z | 128.389° SE | 2026-04-28 10:39:29.082Z | 78.219° E | 27.409° | 2026-04-28 10:43:29.082Z | 22.83° NE |
| 7 mins | 2026-04-28 12:17:29.082Z | 227.689° WSW | 2026-04-28 12:20:29.082Z | 273.574° WNW | 25.832° | 2026-04-28 12:24:29.082Z | 331.562° NNW |
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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