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, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 CZ-4B DEB
1 40532U 13057E   26170.32984624  .00002339  00000-0  42072-3 0  9999
2 40532  74.8663 191.4446 0184154 314.9765  43.6597 14.56672395591802

Epoch: 2026-06-19T07:54Z

TLE epoch observation values (Epoch: 2026-06-19T07:54:58.715Z)

Latitude

0.00003°

Longitude

165.13959°

Altitude

613.423 km

Speed

7.602 km/s

True Right ascension

12h 45m 46s

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

21:35:23

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

831.843 km

Perigee altitude

571.095 km

Semi-major axis

7,079.606 km

Eccentricity

0.01842

Inclination

74.8663°

RAAN

191.4446°

Arg. of periapsis

314.9765°

True anomaly

45.14105°

Mean anomaly

43.6597°

Eccentric anomaly

44.3979°

Mean motion

3.64359 °/min

Orbital period

98.8 mins

BSTAR

0.00042072

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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.
9 mins	2026-06-22 12:18:21.481Z	345.236° N	2026-06-22 12:22:21.481Z	24.433° NE	44.276°	2026-06-22 12:27:21.481Z	159.402° S
5 mins	2026-06-23 01:04:21.481Z	125.538° SE	2026-06-23 01:06:21.481Z	91.304° ESE	20.872°	2026-06-23 01:09:21.481Z	50.506° ENE
7 mins	2026-06-23 02:43:21.481Z	236.728° WSW	2026-06-23 02:46:21.481Z	294.111° NW	31.105°	2026-06-23 02:50:21.481Z	358.272° N

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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: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-06-19T07:54:58.715Z)

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: 3 days ago