CZ-5 R/B, 66143

Orbit data source: Space-Track

CZ-5 R/B, 66143 is space debris in HEO originally from a launch on Thu, 23 Oct 2025 UTC launched from the Wenchang Satellite Launch Center (WSC). 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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Identifier
66143, 2025-238B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-5 H5-2, Unknown motor
Mass
5,100 kg wet, 5,100 kg dry
Launch date (UTC)
2025-10-23 (2 months ago)
Launch vehicle
Unknown
Launch site
Wenchang Satellite Launch Center (WSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Step Cyl, 8.0 m
Radar Cross Section
46.821 m²

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago
0 CZ-5 R/B
1 66143U 25238B   25361.09102891  .01013615 -61501-6  23386-2 0  9998
2 66143  16.0403 250.3652 7287648 206.9561  80.7089  2.33676759  1315
Epoch: 2025-12-27T02:11Z
TLE epoch observation values (Epoch: 2025-12-27T02:11:04.897Z)
Latitude
0.00013°
Longitude
121.82712°
Altitude
25,743.137 km
Speed
2.864 km/s
True Right ascension
16h 41m 40s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
16:24:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,100.01 km
Perigee altitude
129.592 km
Semi-major axis
23,992.938 km
Eccentricity
0.72876
Inclination
16.0403°
RAAN
250.3652°
Arg. of periapsis
206.9561°
True anomaly
153.06381°
Mean anomaly
80.7089°
Eccentric anomaly
117.68404°
Mean motion
0.58401 °/min
Orbital period
616.43 mins
BSTAR
0.0023386
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Other satellites on launch #238 in the year 2025 (2025-10-23 UTC)

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