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   25348.27632163  .00020137  00000-0  20549-2 0  9992
2 40264  97.8355 245.3321 0058496  21.4551 338.9099 14.89379208595567

Epoch: 2025-12-14T06:37Z

TLE epoch observation values (Epoch: 2025-12-14T06:37:54.188Z)

Latitude

-0.00002°

Longitude

62.66476°

Altitude

564.849 km

Speed

7.599 km/s

True Right ascension

16h 21m 19s

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

18:13:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

637.7 km

Perigee altitude

556.098 km

Semi-major axis

6,975.036 km

Eccentricity

0.00585

Inclination

97.8355°

RAAN

245.3321°

Arg. of periapsis

21.4551°

True anomaly

338.66704°

Mean anomaly

338.9099°

Eccentric anomaly

338.78864°

Mean motion

3.72583 °/min

Orbital period

96.62 mins

BSTAR

0.0020549

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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	2025-12-15 05:46:06.633Z	27.415° NE	2025-12-15 05:50:06.633Z	111.263° ESE	35.024°	2025-12-15 05:53:06.633Z	168.175° S
5 mins	2025-12-15 16:39:06.633Z	109.204° ESE	2025-12-15 16:41:06.633Z	60.8° ENE	24.797°	2025-12-15 16:44:06.633Z	11.734° NNE
4 mins	2025-12-15 18:15:06.633Z	238.185° WSW	2025-12-15 18:16:06.633Z	257.466° W	18.71°	2025-12-15 18:19:06.633Z	310.222° NW

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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: 2025-12-14T06:37:54.188Z)

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