CZ-2C DEB, 40289

Orbit data source: Space-Track

CZ-2C DEB, 40289 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/40289?theme=dark&initialShowStats=false

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Identifier

40289, 2014-066D

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 (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: 11 hours ago

TLE from 11 hours ago

0 CZ-2C DEB
1 40289U 14066D   25351.71572764  .00007732  00000-0  10761-2 0  9991
2 40289  98.4943 255.0845 0071939   7.2973 352.9265 14.76309610591462

Epoch: 2025-12-17T17:10Z

TLE epoch observation values (Epoch: 2025-12-17T17:10:38.868Z)

Latitude

0.00005°

Longitude

-89.15906°

Altitude

593.88 km

Speed

7.59 km/s

True Right ascension

17h 00m 20s

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

02:30:25

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

688.544 km

Perigee altitude

587.596 km

Semi-major axis

7,016.207 km

Eccentricity

0.00719

Inclination

98.4943°

RAAN

255.0845°

Arg. of periapsis

7.2973°

True anomaly

352.82407°

Mean anomaly

352.9265°

Eccentric anomaly

352.87538°

Mean motion

3.69309 °/min

Orbital period

97.48 mins

BSTAR

0.0010761

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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.
8 mins	2025-12-18 06:44:50.703Z	10.268° NNE	2025-12-18 06:48:50.703Z	308.643° NW	44.361°	2025-12-18 06:52:50.703Z	199.682° SSW
6 mins	2025-12-18 17:42:50.703Z	164.771° S	2025-12-18 17:45:50.703Z	350.575° N	43.437°	2025-12-18 17:48:50.703Z	347.107° 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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View CZ-2C DEB, 40289 on Gunter's Space Page

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CZ-2C DEB, 40289

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2025-12-17T17:10:38.868Z)

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, 40289 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago