CZ-4C DEB, 64783
Orbit data source: Space-Track
CZ-4C DEB, 64783 is space debris in LEO originally from a launch on Thu, 03 Jul 2025 UTC launched from the Xichang Space Center, China (XSC). 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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64783 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
Unknown
Mass
1 kg wet, 1 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 CZ-4C DEB
1 64783U 25145C 25239.90994620 .00429860 00000-0 14017+0 0 9996
2 64783 10.9689 79.0709 0024267 190.0541 169.9202 14.35254692 7159Epoch: 2025-08-27T21:50Z
TLE epoch observation values (Epoch: 2025-08-27T21:50:19.351Z)
Latitude
0°
Longitude
135.10976°
Altitude
788.46 km
Speed
7.454 km/s
True Right ascension
05h 16m 17s
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
00:52:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
797.422 km
Perigee altitude
762.681 km
Semi-major axis
7,158.188 km
Eccentricity
0.00243
Inclination
10.9689°
RAAN
79.0709°
Arg. of periapsis
190.0541°
True anomaly
169.96872°
Mean anomaly
169.9202°
Eccentric anomaly
169.94448°
Mean motion
3.58376 °/min
Orbital period
100.45 mins
BSTAR
0.14017
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Other satellites on launch #145 in the year 2025 (2025-07-03 UTC)
CZ-4C DEB Visibility
Observer location: undefined°, undefined°
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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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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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