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, 6.4 m

Radar Cross Section

32.704 m², Large (>1 m²)

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Last TLE update: 5 days ago

TLE from 5 days ago

0 CZ-3A R/B
1 43492U 18050B   26256.30779855  .00000746  00000-0  10894-2 0  9992
2 43492  24.6062  46.3956 7225100 297.3136   8.4264  2.30558766 68218

Epoch: 2026-09-13T07:23Z

TLE epoch observation values (Epoch: 2026-09-13T07:23:13.794Z)

Latitude

-0.00172°

Longitude

-56.70894°

Altitude

2,282.737 km

Speed

8.693 km/s

True Right ascension

03h 05m 36s

True Declination

0° 00' 06"

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

20:43:29

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,319.926 km

Perigee altitude

339.267 km

Semi-major axis

24,207.733 km

Eccentricity

0.72251

Inclination

24.6062°

RAAN

46.3956°

Arg. of periapsis

297.3136°

True anomaly

62.95906°

Mean anomaly

8.4264°

Eccentric anomaly

27.6149°

Mean motion

0.57625 °/min

Orbital period

624.73 mins

BSTAR

0.0010894

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

FENGYUN 2H DEB, 43645

FENGYUN 2H, 43491

FENGYUN 2H AKM, 43497

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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.
572 mins	2026-09-18 12:22:36.320Z	211.967° SW	2026-09-18 18:06:36.320Z	153.134° SSE	63.404°	2026-09-18 21:54:36.320Z	152.882° SSE

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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: 5 days ago

TLE from 5 days ago

TLE epoch observation values (Epoch: 2026-09-13T07:23:13.794Z)

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: 5 days ago