CZ-2C DEB, 40265

Orbit data source: Space-Track

CZ-2C DEB, 40265 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/40265?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40265, 2014-059E

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 40265U 14059E   26171.27884547  .00001661  00000-0  53978-3 0  9997
2 40265  97.9259 244.5158 0163865 105.7314 256.2013 14.32585359608603

Epoch: 2026-06-20T06:41Z

TLE epoch observation values (Epoch: 2026-06-20T06:41:32.248Z)

Latitude

-0.00006°

Longitude

-124.36431°

Altitude

815.857 km

Speed

7.43 km/s

True Right ascension

16h 18m 03s

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

00:50:38

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

897.507 km

Perigee altitude

662.906 km

Semi-major axis

7,158.344 km

Eccentricity

0.01639

Inclination

97.9259°

RAAN

244.5158°

Arg. of periapsis

105.7314°

True anomaly

254.38691°

Mean anomaly

256.2013°

Eccentric anomaly

255.29318°

Mean motion

3.58364 °/min

Orbital period

100.46 mins

BSTAR

0.00053978

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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.
8 mins	2026-06-22 17:56:04.288Z	6.939° NNE	2026-06-22 18:00:04.288Z	246.317° WSW	42.939°	2026-06-22 18:04:04.288Z	201.283° SSW
4 mins	2026-06-23 03:36:04.288Z	86.712° E	2026-06-23 03:38:04.288Z	58.635° ENE	14.551°	2026-06-23 03:40:04.288Z	32.469° NE
8 mins	2026-06-23 05:13:04.288Z	184.721° SSW	2026-06-23 05:17:04.288Z	280.586° WNW	39.26°	2026-06-23 05:21:04.288Z	337.933° N

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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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CZ-2C DEB, 40265

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: 2026-06-20T06:41:32.248Z)

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, 40265 on other resources

Documentation

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