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
Country
CN / PRCRelated business
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 & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 CZ-4C R/B
1 64754U 25145B 25242.81134574 .00001160 00000-0 12209-3 0 9996
2 64754 10.9859 41.4582 0121659 50.3689 310.7213 14.56388992 8414Epoch: 2025-08-30T19:28Z
TLE epoch observation values (Epoch: 2025-08-30T19:28:20.271Z)
Latitude
-0.00001°
Longitude
130.1334°
Altitude
646.403 km
Speed
7.567 km/s
True Right ascension
02h 45m 49s
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
00:53:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
796.989 km
Perigee altitude
624.504 km
Semi-major axis
7,088.883 km
Eccentricity
0.01217
Inclination
10.9859°
RAAN
41.4582°
Arg. of periapsis
50.3689°
True anomaly
309.65419°
Mean anomaly
310.7213°
Eccentric anomaly
310.1888°
Mean motion
3.63644 °/min
Orbital period
99 mins
BSTAR
0.00012209
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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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