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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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 (11 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, Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 CZ-2C DEB
1 40265U 14059E   26061.74597764  .00002410  00000-0  78471-3 0  9997
2 40265  97.9309 144.2657 0163716  75.3948 286.5329 14.32159047592923

Epoch: 2026-03-02T17:54Z

TLE epoch observation values (Epoch: 2026-03-02T17:54:12.468Z)

Latitude

0.00008°

Longitude

75.17877°

Altitude

755.88 km

Speed

7.493 km/s

True Right ascension

09h 37m 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

09:34:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

898.845 km

Perigee altitude

664.412 km

Semi-major axis

7,159.765 km

Eccentricity

0.01637

Inclination

97.9309°

RAAN

144.2657°

Arg. of periapsis

75.3948°

True anomaly

284.72418°

Mean anomaly

286.5329°

Eccentric anomaly

285.62956°

Mean motion

3.58257 °/min

Orbital period

100.49 mins

BSTAR

0.00078471

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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	2026-03-03 17:57:46.853Z	28.303° NE	2026-03-03 18:00:46.853Z	93.011° ESE	39.49°	2026-03-03 18:05:46.853Z	178.476° S
4 mins	2026-03-03 19:38:46.853Z	312.488° NW	2026-03-03 19:39:46.853Z	298.055° NW	15.504°	2026-03-03 19:42:46.853Z	259.466° W
7 mins	2026-03-04 05:14:46.853Z	155.832° SSE	2026-03-04 05:17:46.853Z	104.346° ESE	42.88°	2026-03-04 05:21:46.853Z	353.516° 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: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-03-02T17:54:12.468Z)

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: 12 hours ago