CZ-8A R/B, 65052

Orbit data source: Space-Track

CZ-8A R/B, 65052 is space debris in LEO originally from a launch on Wed, 30 Jul 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
65052, 2025-162K
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-8A STAGE 2, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2025-07-30 (4 months ago)
Launch vehicle
Unknown
Launch site
Wenchang Satellite Launch Center (WSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 8.0 m
Radar Cross Section
36.967 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago
0 CZ-8A R/B
1 65052U 25162K   25342.27765198  .00000299  00000-0  16351-3 0  9994
2 65052  50.0003 177.7168 0118319 184.8877 175.0891 14.30613175 18754
Epoch: 2025-12-08T06:39Z
TLE epoch observation values (Epoch: 2025-12-08T06:39:49.131Z)
Latitude
-0.00006°
Longitude
0.48305°
Altitude
874.714 km
Speed
7.372 km/s
True Right ascension
11h 50m 52s
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
21:51:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
875.24 km
Perigee altitude
705.605 km
Semi-major axis
7,168.559 km
Eccentricity
0.01183
Inclination
50.0003°
RAAN
177.7168°
Arg. of periapsis
184.8877°
True anomaly
175.20348°
Mean anomaly
175.0891°
Eccentric anomaly
175.14646°
Mean motion
3.57598 °/min
Orbital period
100.67 mins
BSTAR
0.00016351
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