CZ-3B R/B, 62375

Orbit data source: Space-Track

CZ-3B R/B, 62375 is space debris in HEO originally from a launch on Fri, 20 Dec 2024 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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Identifier
62375, 2024-246B
Orbit
HEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
CZ-3A STAGE 3, Unknown motor
Mass
~2,800 kg wet, ~2,800 kg dry
Launch date (UTC)
2024-12-20 (2 years ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.4 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CZ-3B R/B
1 62375U 24246B   26299.06292015  .00582624  69055-6  10177-2 0  9990
2 62375  27.9814 238.3842 5434016 173.2880 199.0486  5.08604252 23541
Epoch: 2026-10-26T01:30Z
TLE epoch observation values (Epoch: 2026-10-26T01:30:36.300Z)
Latitude
0.00006°
Longitude
-178.72602°
Altitude
15,485.905 km
Speed
2.925 km/s
True Right ascension
15h 53m 29s
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
22:58:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
15,671.455 km
Perigee altitude
144.992 km
Semi-major axis
14,286.361 km
Eccentricity
0.5434
Inclination
27.9814°
RAAN
238.3842°
Arg. of periapsis
173.288°
True anomaly
186.74979°
Mean anomaly
199.0486°
Eccentric anomaly
192.37576°
Mean motion
1.27104 °/min
Orbital period
283.23 mins
BSTAR
0.0010177
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Other satellites on launch #246 in the year 2024 (2024-12-20 UTC)

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