CZ-4B DEB, 40530

Orbit data source: Space-Track

CZ-4B DEB, 40530 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/40530?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40530, 2013-057C

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 (12 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: 11 hours ago

TLE from 11 hours ago

0 CZ-4B DEB
1 40530U 13057C   26105.41445373  .00001491  00000-0  25875-3 0  9998
2 40530  75.0533   9.2749 0172863 297.5908  60.7798 14.59637443583217

Epoch: 2026-04-15T09:56Z

TLE epoch observation values (Epoch: 2026-04-15T09:56:48.802Z)

Latitude

-0.00001°

Longitude

16.49487°

Altitude

638.981 km

Speed

7.57 km/s

True Right ascension

00h 37m 05s

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

03:24:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

814.071 km

Perigee altitude

569.643 km

Semi-major axis

7,069.994 km

Eccentricity

0.01729

Inclination

75.0533°

RAAN

9.2749°

Arg. of periapsis

297.5908°

True anomaly

62.52675°

Mean anomaly

60.7798°

Eccentric anomaly

61.65145°

Mean motion

3.65102 °/min

Orbital period

98.6 mins

BSTAR

0.00025875

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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.
10 mins	2026-04-16 04:35:21.326Z	350.467° N	2026-04-16 04:40:21.326Z	52.768° ENE	39.81°	2026-04-16 04:45:21.326Z	146.791° SSE
5 mins	2026-04-16 06:18:21.326Z	293.778° NW	2026-04-16 06:20:21.326Z	268.57° W	16.807°	2026-04-16 06:23:21.326Z	231.59° WSW
4 mins	2026-04-16 17:21:21.326Z	112.4° ESE	2026-04-16 17:22:21.326Z	98.702° ESE	15.019°	2026-04-16 17:25:21.326Z	60.497° ENE
8 mins	2026-04-16 18:59:21.326Z	220.013° SW	2026-04-16 19:02:21.326Z	283.41° WNW	39.04°	2026-04-16 19:07:21.326Z	8.252° 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, 40530 on other resources

View CZ-4B DEB, 40530 on Heavens-Above

View CZ-4B DEB, 40530 on Keep Track

View CZ-4B DEB, 40530 on Celestrak

View CZ-4B DEB, 40530 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, 40530

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-04-15T09:56:48.802Z)

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, 40530 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago