CZ-4B DEB, 40532

Orbit data source: Space-Track

CZ-4B DEB, 40532 is space debris in LEO originally from a launch on Fri, 25 Oct 2013 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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/40532?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40532, 2013-057E

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2013-10-25 (13 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.050 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 17 hours ago

TLE from 17 hours ago

0 CZ-4B DEB
1 40532U 13057E   26283.56184055  .00001862  00000-0  33417-3 0  9993
2 40532  74.8688 347.2394 0180369  56.3079 305.5140 14.57221568608290

Epoch: 2026-10-10T13:29Z

TLE epoch observation values (Epoch: 2026-10-10T13:29:03.023Z)

Latitude

0.00001°

Longitude

125.80961°

Altitude

632.196 km

Speed

7.581 km/s

True Right ascension

23h 08m 57s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

00:46:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

827.351 km

Perigee altitude

572.027 km

Semi-major axis

7,077.826 km

Eccentricity

0.01804

Inclination

74.8688°

RAAN

347.2394°

Arg. of periapsis

56.3079°

True anomaly

303.80955°

Mean anomaly

305.514°

Eccentric anomaly

304.664°

Mean motion

3.64496 °/min

Orbital period

98.77 mins

BSTAR

0.00033417

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Other satellites on launch #57 in the year 2013 (2013-10-25 UTC)

CZ-4B R/B, 39359 (Decayed)

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CZ-4B DEB 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.
7 mins	2026-10-11 14:44:23.447Z	13.373° NNE	2026-10-11 14:47:23.447Z	56.636° ENE	23.045°	2026-10-11 14:51:23.447Z	114.785° SE
7 mins	2026-10-11 16:25:23.447Z	314.161° NW	2026-10-11 16:28:23.447Z	256.341° W	35.095°	2026-10-11 16:32:23.447Z	195.988° SSW
7 mins	2026-10-12 05:09:23.447Z	182.455° SSW	2026-10-12 05:12:23.447Z	117.391° SE	61.557°	2026-10-12 05:16:23.447Z	25.211° NE

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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-4B DEB, 40532 on other resources

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View CZ-4B DEB, 40532 on Keep Track

View CZ-4B DEB, 40532 on Celestrak

View CZ-4B DEB, 40532 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-4B DEB, 40532

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-10-10T13:29:03.023Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #57 in the year 2013 (2013-10-25 UTC)

CZ-4B DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4B DEB, 40532 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago