CZ-4C DEB, 43424

Orbit data source: Space-Track

CZ-4C DEB, 43424 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/43424?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43424, 2015-040C

Orbit

SSO

Last TLE update

17 hours ago

Origin

China National Space Administration (CN / PRC)

Manufacturer

SAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2015-08-27 (10 years ago)

Launch vehicle

Unknown

Launch site

Taiyaun Space Center, China (TSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 17 hours ago

0 CZ-4C DEB
1 43424U 15040C   25215.72014495 -.00000014  00000-0  79615-4 0  9992
2 43424 100.2757 192.7704 0150620 314.9079  43.9887 13.10500781470644

Epoch: 2025-08-03T17:17Z

TLE epoch observation values (Epoch: 2025-08-03T17:17:00.523Z)

Latitude

-0.00011°

Longitude

-19.01967°

Altitude

1,142.413 km

Speed

7.321 km/s

True Right ascension

12h 51m 04s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-4.2197°

Longitude

160.91669°

Altitude

1,295.741 km

Speed

7.175 km/s

Apparent Right ascension

01h 17m 03s

Apparent Declination

-59° 00' 12"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:35:56

Azimuth

174.658° S

Elevation

-9.287°

Doppler factor

Orbital elements

Apogee altitude

1,333.028 km

Perigee altitude

1,104.184 km

Semi-major axis

7,596.743 km

Eccentricity

0.01506

Inclination

100.2757°

RAAN

192.7704°

Arg. of periapsis

314.9079°

True anomaly

45.20378°

Mean anomaly

43.9887°

Eccentric anomaly

44.59459°

Mean motion

3.27795 °/min

Orbital period

109.82 mins

BSTAR

0.000079615

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

YAOGAN 27, 40878

CZ-4C R/B, 40879

CZ-4C DEB, 43425

CZ-4C 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.
14 mins	2025-08-04 12:11:24.264Z	4.415° NNE	2025-08-04 12:18:24.264Z	293.693° NW	37.666°	2025-08-04 12:25:24.264Z	222.457° SW
10 mins	2025-08-04 20:55:24.264Z	106.181° ESE	2025-08-04 21:00:24.264Z	57.655° ENE	23.107°	2025-08-04 21:05:24.264Z	10.763° NNE
12 mins	2025-08-04 22:42:24.264Z	177.97° S	2025-08-04 22:47:24.264Z	235.34° WSW	42.033°	2025-08-04 22:54:24.264Z	337.767° N
11 mins	2025-08-05 10:14:24.264Z	45.47° ENE	2025-08-05 10:19:24.264Z	94.956° ESE	26.015°	2025-08-05 10:25:24.264Z	149.878° SSE

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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Authenticating...

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Check out CZ-4C DEB, 43424 on other resources

View CZ-4C DEB, 43424 on Heavens-Above

View CZ-4C DEB, 43424 on Keep Track

View CZ-4C DEB, 43424 on Celestrak

View CZ-4C DEB, 43424 on Gunter's Space Page

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