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 (1 year ago)
Launch vehicle
Unknown
Launch site
Xichang Space Center, China (XSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Nozzle, 6.2 m
Radar Cross Section
32.704 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 CZ-3B R/B
1 62375U 24246B   26046.18687414  .00221680  38116-6  11716-2 0  9990
2 62375  28.0006  96.1659 6102614 176.2963 192.1484  4.00283642 12439
Epoch: 2026-02-15T04:29Z
TLE epoch observation values (Epoch: 2026-02-15T04:29:05.925Z)
Latitude
0.00003°
Longitude
-116.29563°
Altitude
20,509.689 km
Speed
2.421 km/s
True Right ascension
06h 24m 42s
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
20:12:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
20,608.266 km
Perigee altitude
153.5 km
Semi-major axis
16,759.02 km
Eccentricity
0.61026
Inclination
28.0006°
RAAN
96.1659°
Arg. of periapsis
176.2963°
True anomaly
183.71976°
Mean anomaly
192.1484°
Eccentric anomaly
187.55265°
Mean motion
1.00039 °/min
Orbital period
359.86 mins
BSTAR
0.0011716
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Other satellites on launch #246 in the year 2024 (2024-12-20 UTC)

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