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: 1 day ago

TLE from 1 day ago

0 CZ-4B DEB
1 40532U 13057E   26296.05641288  .00002614  00000-0  46650-3 0  9996
2 40532  74.8680 324.6967 0180530  27.5935 333.4672 14.57277861610119

Epoch: 2026-10-23T01:21Z

TLE epoch observation values (Epoch: 2026-10-23T01:21:14.072Z)

Latitude

-0.00012°

Longitude

-87.0944°

Altitude

590.757 km

Speed

7.625 km/s

True Right ascension

21h 38m 47s

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

07:30:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

827.279 km

Perigee altitude

571.734 km

Semi-major axis

7,077.644 km

Eccentricity

0.01805

Inclination

74.868°

RAAN

324.6967°

Arg. of periapsis

27.5935°

True anomaly

332.5241°

Mean anomaly

333.4672°

Eccentric anomaly

332.99757°

Mean motion

3.64511 °/min

Orbital period

98.76 mins

BSTAR

0.0004665

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

CZ-4B DEB, 40531

CZ-4B DEB, 40530

SJ-16, 39358

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

CZ-4B DEB, 40533

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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.
8 mins	2026-10-24 12:29:48.902Z	8.462° NNE	2026-10-24 12:33:48.902Z	72.921° E	30.382°	2026-10-24 12:37:48.902Z	125.26° SE
7 mins	2026-10-24 14:10:48.902Z	310.975° NW	2026-10-24 14:13:48.902Z	262.66° W	30.444°	2026-10-24 14:17:48.902Z	204.439° SW
7 mins	2026-10-25 02:54:48.902Z	191.798° SSW	2026-10-25 02:57:48.902Z	107.996° ESE	80.474°	2026-10-25 03:01:48.902Z	20.077° NNE

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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

View CZ-4B DEB, 40532 on Heavens-Above

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: 1 day ago

TLE from 1 day ago

TLE epoch observation values (Epoch: 2026-10-23T01:21:14.072Z)

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: 1 day ago