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 (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: 13 hours ago

TLE from 13 hours ago

0 CZ-2C DEB
1 40264U 14059D   26061.71931272  .00019157  00000-0  18017-2 0  9994
2 40264  97.8311 323.2185 0054041 118.6839 241.9828 14.92809759607259

Epoch: 2026-03-02T17:15Z

TLE epoch observation values (Epoch: 2026-03-02T17:15:48.619Z)

Latitude

0.00002°

Longitude

-96.24277°

Altitude

610.069 km

Speed

7.545 km/s

True Right ascension

21h 32m 52s

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

09:33:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

623.836 km

Perigee altitude

548.564 km

Semi-major axis

6,964.337 km

Eccentricity

0.0054

Inclination

97.8311°

RAAN

323.2185°

Arg. of periapsis

118.6839°

True anomaly

241.43785°

Mean anomaly

241.9828°

Eccentric anomaly

241.71015°

Mean motion

3.73442 °/min

Orbital period

96.4 mins

BSTAR

0.0018017

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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	2026-03-03 06:41:49.834Z	353.172° N	2026-03-03 06:44:49.834Z	286.635° WNW	33.093°	2026-03-03 06:47:49.834Z	221.36° SW
6 mins	2026-03-03 17:31:49.834Z	178.572° S	2026-03-03 17:33:49.834Z	211.881° SW	41.319°	2026-03-03 17:37:49.834Z	341.533° 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, 40264

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 13 hours ago

TLE from 13 hours ago

TLE epoch observation values (Epoch: 2026-03-02T17:15:48.619Z)

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: 13 hours ago