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

Last TLE update

21 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2013-10-25 (12 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 21 hours ago

0 CZ-4B DEB
1 40532U 13057E   25174.83053842  .00003715  00000-0  70500-3 0  9993
2 40532  74.8693 119.8338 0188227  55.5652 306.3143 14.53705097539369

Epoch: 2025-06-23T19:55Z

TLE epoch observation values (Epoch: 2025-06-23T19:55:58.519Z)

Latitude

-0.00006°

Longitude

-91.39523°

Altitude

638.846 km

Speed

7.58 km/s

True Right ascension

07h 59m 20s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-59.74563°

Longitude

-120.43705°

Altitude

794.525 km

Speed

7.425 km/s

Apparent Right ascension

13h 22m 34s

Apparent Declination

-77° 23' 51"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

04:18:49

Azimuth

166.819° S

Elevation

-48.285°

Doppler factor

Orbital elements

Apogee altitude

844.545 km

Perigee altitude

577.667 km

Semi-major axis

7,089.243 km

Eccentricity

0.01882

Inclination

74.8693°

RAAN

119.8338°

Arg. of periapsis

55.5652°

True anomaly

Unknown

Mean anomaly

306.3143°

Eccentric anomaly

Unknown

Mean motion

3.63616 °/min

Orbital period

99.01 mins

BSTAR

0.000705

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

CZ-4B DEB Visibility forecast

Observer location: undefined°, undefined°

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.
6 mins	2025-06-24 20:49:52.627Z	160.194° S	2025-06-24 20:52:52.627Z	106.675° ESE	27.733°	2025-06-24 20:55:52.627Z	44.995° NE
4 mins	2025-06-24 22:31:52.627Z	263.42° W	2025-06-24 22:33:52.627Z	297.931° NW	17.996°	2025-06-24 22:35:52.627Z	332.443° NNW
7 mins	2025-06-25 07:10:52.627Z	5.691° NNE	2025-06-25 07:13:52.627Z	81.463° E	35.726°	2025-06-25 07:17:52.627Z	140.976° SSE
4 mins	2025-06-25 08:52:52.627Z	279.696° WNW	2025-06-25 08:53:52.627Z	264.646° W	16.615°	2025-06-25 08:56:52.627Z	225.655° WSW

Authenticating...

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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

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