CZ-4C DEB, 39016

Orbit data source: Space-Track

CZ-4C DEB, 39016 is space debris in LEO originally from a launch on Sun, 25 Nov 2012 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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https://www.satcat.com/sats-embedded/39016?theme=dark&initialShowStats=false

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Identifier

39016, 2012-066F

Orbit

LEO

Country

CN / PRC

Related business

China National Space Administration (CN)

Manufacturer

CAST

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2012-11-25 (14 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 3.4 m

Radar Cross Section

Large (>1 m²)

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

TLE from 2 days ago

0 CZ-4C DEB
1 39016U 12066F   26171.41503090 -.00000075  00000-0  15269-4 0  9993
2 39016  63.3550 295.2885 0444215  28.2751 334.1632 13.45323028666222

Epoch: 2026-06-20T09:57Z

TLE epoch observation values (Epoch: 2026-06-20T09:57:38.669Z)

Latitude

-0.00011°

Longitude

-122.75266°

Altitude

795.659 km

Speed

7.602 km/s

True Right ascension

19h 41m 09s

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

00:39:54

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,420.02 km

Perigee altitude

756.675 km

Semi-major axis

7,466.485 km

Eccentricity

0.04442

Inclination

63.355°

RAAN

295.2885°

Arg. of periapsis

28.2751°

True anomaly

331.829°

Mean anomaly

334.1632°

Eccentric anomaly

333.00804°

Mean motion

3.3641 °/min

Orbital period

107.01 mins

BSTAR

0.000015269

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Other satellites on launch #66 in the year 2012 (2012-11-25 UTC)

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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.
6 mins	2026-06-22 15:57:22.048Z	3.742° NNE	2026-06-22 16:00:22.048Z	32.989° NE	14.021°	2026-06-22 16:03:22.048Z	59.375° ENE
12 mins	2026-06-22 17:47:22.048Z	341.281° N	2026-06-22 17:52:22.048Z	60.187° ENE	38.359°	2026-06-22 17:59:22.048Z	126.283° SE
12 mins	2026-06-22 19:37:22.048Z	302.835° NW	2026-06-22 19:42:22.048Z	248.031° W	29.953°	2026-06-22 19:49:22.048Z	184.864° SSW
9 mins	2026-06-23 09:27:22.048Z	202.836° SW	2026-06-23 09:31:22.048Z	109.689° ESE	43.578°	2026-06-23 09:36:22.048Z	38.02° NE
5 mins	2026-06-23 11:20:22.048Z	295.845° NW	2026-06-23 11:22:22.048Z	324.143° NNW	18.438°	2026-06-23 11:25:22.048Z	1.65° 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-4C DEB, 39016 on other resources

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View CZ-4C DEB, 39016 on Keep Track

View CZ-4C DEB, 39016 on Celestrak

View CZ-4C DEB, 39016 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, 39016

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: 2026-06-20T09:57:38.669Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #66 in the year 2012 (2012-11-25 UTC)

CZ-4C DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-4C DEB, 39016 on other resources

Documentation

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