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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Iframe URL

https://www.satcat.com/sats-embedded/62375?theme=dark&initialShowStats=false

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Identifier

62375, 2024-246B

Orbit

HEO

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

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)

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Last TLE update: 1 day ago

TLE from 1 day ago

0 CZ-3B R/B
1 62375U 24246B   25345.74540086  .00504198  41090-8  10408-2 0  9998
2 62375  27.9152 142.6811 6493732 100.2952 333.7383  3.42783516  9960

Epoch: 2025-12-11T17:53Z

TLE epoch observation values (Epoch: 2025-12-11T17:53:22.634Z)

Latitude

0.00002°

Longitude

153.60779°

Altitude

5,767.427 km

Speed

6.647 km/s

True Right ascension

09h 30m 35s

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

17:13:04

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

24,273.875 km

Perigee altitude

137.924 km

Semi-major axis

18,584.037 km

Eccentricity

0.64937

Inclination

27.9152°

RAAN

142.6811°

Arg. of periapsis

100.2952°

True anomaly

259.8357°

Mean anomaly

333.7383°

Eccentric anomaly

302.28346°

Mean motion

0.85671 °/min

Orbital period

420.21 mins

BSTAR

0.0010408

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Other satellites on launch #246 in the year 2024 (2024-12-20 UTC)

TJS-12, 62374

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CZ-3B R/B Visibility forecast

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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.
49 mins	2025-12-13 11:15:39.820Z	214.983° SW	2025-12-13 11:55:39.820Z	179.08° S	21.028°	2025-12-13 12:04:39.820Z	133.605° SE

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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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Check out CZ-3B R/B, 62375 on other resources

View CZ-3B R/B, 62375 on Heavens-Above

View CZ-3B R/B, 62375 on Keep Track

View CZ-3B R/B, 62375 on Celestrak

View CZ-3B R/B, 62375 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

CZ-3B R/B, 62375

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2025-12-11T17:53:22.634Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #246 in the year 2024 (2024-12-20 UTC)

CZ-3B R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-3B R/B, 62375 on other resources

Documentation

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