CZ-4B R/B, 64201 (Decayed)
Orbit data source: Space-Track
CZ-4B R/B, 64201 was space debris in LEO originally from a launch on Thu, 29 May 2025 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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64201 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed 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
Cyl, 8.0 m
Radar Cross Section
14.536 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 CZ-4B R/B
1 64201U 25115C 25279.28237539 .09561758 25501-5 14998-3 0 9994
2 64201 97.3911 4.6412 0023825 252.3546 107.5155 16.46249367 20519Epoch: 2025-10-06T06:46Z
TLE epoch observation values (Epoch: 2025-10-06T06:46:37.233Z)
Latitude
-0.00004°
Longitude
-112.20179°
Altitude
157.206 km
Speed
7.809 km/s
True Right ascension
00h 18m 33s
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
07:11:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
161.574 km
Perigee altitude
130.486 km
Semi-major axis
6,524.167 km
Eccentricity
0.00238
Inclination
97.3911°
RAAN
4.6412°
Arg. of periapsis
252.3546°
True anomaly
107.77562°
Mean anomaly
107.5155°
Eccentric anomaly
107.64558°
Mean motion
4.11866 °/min
Orbital period
87.41 mins
BSTAR
0.00014998
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Other satellites on launch #115 in the year 2025 (2025-05-29 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-4B R/B Visibility
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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. |
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| This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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