CZ-4C DEB, 43425

Orbit data source: Space-Track

CZ-4C DEB, 43425 is space debris in SSO originally from a launch on Thu, 27 Aug 2015 UTC launched from the Taiyaun Space Center, China (TSC). 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/43425?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43425, 2015-040D

Orbit

SSO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2015-08-27 (11 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

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: 2 days ago

TLE from 2 days ago

0 CZ-4C DEB
1 43425U 15040D   26295.40991325  .00000101  00000-0  32946-3 0  9994
2 43425 100.1689   4.2200 0141831 229.2231 129.6508 13.22633248537361

Epoch: 2026-10-22T09:50Z

TLE epoch observation values (Epoch: 2026-10-22T09:50:16.504Z)

Latitude

-0°

Longitude

-174.19398°

Altitude

1,246.666 km

Speed

7.199 km/s

True Right ascension

00h 16m 52s

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

05:58:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,279.125 km

Perigee altitude

1,064.955 km

Semi-major axis

7,550.177 km

Eccentricity

0.01418

Inclination

100.1689°

RAAN

4.22°

Arg. of periapsis

229.2231°

True anomaly

130.88807°

Mean anomaly

129.6508°

Eccentric anomaly

130.27084°

Mean motion

3.30832 °/min

Orbital period

108.82 mins

BSTAR

0.00032946

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Other satellites on launch #40 in the year 2015 (2015-08-27 UTC)

CZ-4C DEB, 43424

YAOGAN 27, 40878

CZ-4C R/B, 40879

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CZ-4C 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.
13 mins	2026-10-24 16:55:01.770Z	28.692° NE	2026-10-24 17:02:01.770Z	106.573° ESE	42.632°	2026-10-24 17:08:01.770Z	168.641° S
10 mins	2026-10-24 18:44:01.770Z	351.626° N	2026-10-24 18:49:01.770Z	291.306° WNW	35.462°	2026-10-24 18:54:01.770Z	237.736° WSW
11 mins	2026-10-25 03:21:01.770Z	112.059° ESE	2026-10-25 03:26:01.770Z	59.993° ENE	31.513°	2026-10-25 03:32:01.770Z	4.579° NNE
13 mins	2026-10-25 05:07:01.770Z	185.993° SSW	2026-10-25 05:13:01.770Z	268.394° W	55.565°	2026-10-25 05:20:01.770Z	336.003° NNW

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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-4C DEB, 43425 on other resources

View CZ-4C DEB, 43425 on Heavens-Above

View CZ-4C DEB, 43425 on Keep Track

View CZ-4C DEB, 43425 on Celestrak

View CZ-4C DEB, 43425 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-4C DEB, 43425

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-10-22T09:50:16.504Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #40 in the year 2015 (2015-08-27 UTC)

CZ-4C DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4C DEB, 43425 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago