CZ-2C DEB, 40290

Orbit data source: Space-Track

CZ-2C DEB, 40290 is space debris in SSO originally from a launch on Mon, 27 Oct 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/40290?theme=dark&initialShowStats=false

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Identifier

40290, 2014-066E

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)

2014-10-27 (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: 16 hours ago

TLE from 16 hours ago

0 CZ-2C DEB
1 40290U 14066E   26297.19180361  .00015661  00000-0  11144-2 0  9999
2 40290  97.9640 277.9686 0039874 115.0380 245.4993 15.04082644639352

Epoch: 2026-10-24T04:36Z

TLE epoch observation values (Epoch: 2026-10-24T04:36:11.831Z)

Latitude

-0.00004°

Longitude

176.31778°

Altitude

568.933 km

Speed

7.57 km/s

True Right ascension

18h 31m 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

15:41:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

578.965 km

Perigee altitude

523.704 km

Semi-major axis

6,929.472 km

Eccentricity

0.00399

Inclination

97.964°

RAAN

277.9686°

Arg. of periapsis

115.038°

True anomaly

245.08438°

Mean anomaly

245.4993°

Eccentric anomaly

245.29175°

Mean motion

3.76264 °/min

Orbital period

95.68 mins

BSTAR

0.0011144

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Other satellites on launch #66 in the year 2014 (2014-10-27 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	2026-10-24 22:17:58.965Z	133.347° SE	2026-10-24 22:20:58.965Z	77.029° E	33.202°	2026-10-24 22:23:58.965Z	11.959° NNE
6 mins	2026-10-25 11:30:58.965Z	27.21° NE	2026-10-25 11:33:58.965Z	133.632° SE	51.279°	2026-10-25 11:36:58.965Z	179.136° S

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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, 40290

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 16 hours ago

TLE from 16 hours ago

TLE epoch observation values (Epoch: 2026-10-24T04:36:11.831Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #66 in the year 2014 (2014-10-27 UTC)

CZ-2C DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-2C DEB, 40290 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 16 hours ago