CZ-6A DEB, 64654
Orbit data source: Space-Track
CZ-6A DEB, 64654 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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64654 intel report (Beta)
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Edit Public Description
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, 1.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CZ-6A DEB
1 64654U 24140AEU 25350.20979808 .00002099 00000-0 10387-2 0 9995
2 64654 88.3203 256.8280 0081860 60.3207 300.6098 14.15203695 59313Epoch: 2025-12-16T05:02Z
TLE epoch observation values (Epoch: 2025-12-16T05:02:06.554Z)
Latitude
0.00001°
Longitude
96.2034°
Altitude
814.923 km
Speed
7.461 km/s
True Right ascension
17h 07m 18s
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
09:25:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
897.658 km
Perigee altitude
779.506 km
Semi-major axis
7,216.719 km
Eccentricity
0.00819
Inclination
88.3203°
RAAN
256.828°
Arg. of periapsis
60.3207°
True anomaly
299.79827°
Mean anomaly
300.6098°
Eccentric anomaly
300.20445°
Mean motion
3.54025 °/min
Orbital period
101.69 mins
BSTAR
0.0010387
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-17 18:29:39.728Z | 186.241° SSW | 2025-12-17 18:33:39.728Z | 321.568° NNW | 43.182° | 2025-12-17 18:37:39.728Z | 356.167° N |
| 7 mins | 2025-12-18 05:08:39.728Z | 36.136° NE | 2025-12-18 05:11:39.728Z | 78.396° E | 23.362° | 2025-12-18 05:15:39.728Z | 131.853° SE |
| 8 mins | 2025-12-18 06:50:39.728Z | 331.017° NNW | 2025-12-18 06:53:39.728Z | 278.368° WNW | 31.274° | 2025-12-18 06:58:39.728Z | 211.964° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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