CZ-2C DEB, 40266

Orbit data source: Space-Track

CZ-2C DEB, 40266 is space debris in SSO originally from a launch on Sun, 28 Sep 2014 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/40266?theme=dark&initialShowStats=false

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Identifier

40266, 2014-059F

Orbit

SSO

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

Unknown

Mass

1 kg wet, 1 kg dry

Launch date (UTC)

2014-09-28 (12 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cone, 0.1 m

Radar Cross Section

0.025 m², Medium (>0.1 m² and < 1m²)

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

TLE from 2 days ago

0 CZ-2C DEB
1 40266U 14059F   26171.45072672  .00000938  00000-0  30814-3 0  9996
2 40266  98.3547  80.2705 0158617 210.0564 149.1447 14.33719629609149

Epoch: 2026-06-20T10:49Z

TLE epoch observation values (Epoch: 2026-06-20T10:49:02.788Z)

Latitude

0.00002°

Longitude

9.34371°

Altitude

880.214 km

Speed

7.361 km/s

True Right ascension

05h 21m 04s

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

00:50:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

889.931 km

Perigee altitude

662.963 km

Semi-major axis

7,154.584 km

Eccentricity

0.01586

Inclination

98.3547°

RAAN

80.2705°

Arg. of periapsis

210.0564°

True anomaly

150.06125°

Mean anomaly

149.1447°

Eccentric anomaly

149.60453°

Mean motion

3.58647 °/min

Orbital period

100.38 mins

BSTAR

0.00030814

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Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

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CZ-2C 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 16:35:06.283Z	99.056° ESE	2026-06-22 16:38:06.283Z	63.072° ENE	18.357°	2026-06-22 16:41:06.283Z	26.746° NE
9 mins	2026-06-22 18:13:06.283Z	182.877° SSW	2026-06-22 18:17:06.283Z	273.296° WNW	41.593°	2026-06-22 18:22:06.283Z	339.564° N
8 mins	2026-06-23 06:25:06.283Z	28.909° NE	2026-06-23 06:29:06.283Z	112.914° SE	36.563°	2026-06-23 06:33:06.283Z	173.51° S
4 mins	2026-06-23 08:06:06.283Z	319.759° NNW	2026-06-23 08:08:06.283Z	289.495° WNW	17.155°	2026-06-23 08:10:06.283Z	262.068° W

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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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View CZ-2C DEB, 40266 on Gunter's Space Page

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CZ-2C DEB, 40266

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: 2026-06-20T10:49:02.788Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #59 in the year 2014 (2014-09-28 UTC)

CZ-2C DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-2C DEB, 40266 on other resources

Documentation

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