CZ-2C DEB, 40264

Orbit data source: Space-Track

CZ-2C DEB, 40264 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/40264?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40264, 2014-059D

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)

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Last TLE update: 2 days ago

TLE from 2 days ago

0 CZ-2C DEB
1 40264U 14059D   26171.29864573  .00012877  00000-0  11094-2 0  9998
2 40264  97.8214  72.5151 0051031 114.4572 246.1984 14.96445978623624

Epoch: 2026-06-20T07:10Z

TLE epoch observation values (Epoch: 2026-06-20T07:10:02.991Z)

Latitude

-0.00002°

Longitude

56.48737°

Altitude

595.415 km

Speed

7.554 km/s

True Right ascension

04h 50m 03s

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

21:35:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

610.386 km

Perigee altitude

539.421 km

Semi-major axis

6,953.04 km

Eccentricity

0.0051

Inclination

97.8214°

RAAN

72.5151°

Arg. of periapsis

114.4572°

True anomaly

245.66475°

Mean anomaly

246.1984°

Eccentric anomaly

245.93143°

Mean motion

3.74353 °/min

Orbital period

96.17 mins

BSTAR

0.0011094

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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.
7 mins	2026-06-22 17:03:51.913Z	145.326° SSE	2026-06-22 17:07:51.913Z	50.743° ENE	34.693°	2026-06-22 17:10:51.913Z	1.571° NNE
6 mins	2026-06-23 06:20:51.913Z	11.978° NNE	2026-06-23 06:23:51.913Z	203.317° SW	44.609°	2026-06-23 06:26:51.913Z	194.251° SSW

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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, 40264

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: 2026-06-20T07:10:02.991Z)

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, 40264 on other resources

Documentation

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