CZ-4C R/B, 64754
Orbit data source: Space-Track
CZ-4C R/B, 64754 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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64754 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
1 day ago
Origin
Manufacturer
SAST
Mission
Spacecraft
Bus & Motor
CZ-4 STAGE 3, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & history
TLE from 1 day ago
0 CZ-4C R/B
1 64754U 25145B 25216.57953625 .00000914 00000-0 73030-4 0 9992
2 64754 10.9842 220.1509 0121680 62.8369 298.4213 14.56372019 4587Epoch: 2025-08-04T13:54Z
TLE epoch observation values (Epoch: 2025-08-04T13:54:31.931Z)
Latitude
-0.00001°
Longitude
58.13282°
Altitude
661.856 km
Speed
7.551 km/s
True Right ascension
14h 40m 36s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
-4.44395°
Longitude
-105.17809°
Altitude
754.873 km
Speed
7.452 km/s
Apparent Right ascension
03h 47m 02s
Apparent Declination
-64° 24' 23"
Sunlit
Visualization observer readout
Local Sidereal Time
03:47:30
Azimuth
180.052° SSW
Elevation
-14.323°
Doppler factor
1
Orbital elements
Apogee altitude
797.06 km
Perigee altitude
624.543 km
Semi-major axis
7,088.938 km
Eccentricity
0.01217
Inclination
10.9842°
RAAN
220.1509°
Arg. of periapsis
62.8369°
True anomaly
297.18616°
Mean anomaly
298.4213°
Eccentric anomaly
297.80462°
Mean motion
3.6364 °/min
Orbital period
99 mins
BSTAR
0.00007303
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Other satellites on launch #145 in the year 2025 (2025-07-03 UTC)
CZ-4C R/B 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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