CZ-3A R/B, 43492

Orbit data source: Space-Track

CZ-3A R/B, 43492 is space debris in HEO originally from a launch on Tue, 05 Jun 2018 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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https://www.satcat.com/sats-embedded/43492?theme=dark&initialShowStats=false

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Identifier

43492, 2018-050B

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)

2018-06-05 (8 years 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-3A R/B
1 43492U 18050B   25352.16536928  .00006609  00000-0  29874-2 0  9996
2 43492  23.9838 147.8658 7257457 122.5019 327.6684  2.29819589 62000

Epoch: 2025-12-18T03:58Z

TLE epoch observation values (Epoch: 2025-12-18T03:58:07.905Z)

Latitude

-0.00022°

Longitude

1.29529°

Altitude

12,388.911 km

Speed

5.103 km/s

True Right ascension

09h 51m 24s

True Declination

0° 00' 01"

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

14:42:03

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,487.977 km

Perigee altitude

275.197 km

Semi-major axis

24,259.724 km

Eccentricity

0.72575

Inclination

23.9838°

RAAN

147.8658°

Arg. of periapsis

122.5019°

True anomaly

237.64544°

Mean anomaly

327.6684°

Eccentric anomaly

288.1567°

Mean motion

0.5744 °/min

Orbital period

626.74 mins

BSTAR

0.0029874

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Other satellites on launch #50 in the year 2018 (2018-06-05 UTC)

FENGYUN 2H DEB, 43645

FENGYUN 2H AKM, 43497

FENGYUN 2H, 43491

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CZ-3A 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.
215 mins	2025-12-20 04:50:32.515Z	135.007° SSE	2025-12-20 07:30:32.515Z	137.542° SSE	19.093°	2025-12-20 08:25:32.515Z	115.056° 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-3A R/B, 43492 on other resources

View CZ-3A R/B, 43492 on Heavens-Above

View CZ-3A R/B, 43492 on Keep Track

View CZ-3A R/B, 43492 on Celestrak

View CZ-3A R/B, 43492 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-3A R/B, 43492

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: 2025-12-18T03:58:07.905Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #50 in the year 2018 (2018-06-05 UTC)

CZ-3A R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-3A R/B, 43492 on other resources

Documentation

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