CZ-2C DEB, 40288

Orbit data source: Space-Track

CZ-2C DEB, 40288 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/40288?theme=dark&initialShowStats=false

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Identifier

40288, 2014-066C

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: 17 hours ago

TLE from 17 hours ago

0 CZ-2C DEB
1 40288U 14066C   26283.53610937  .00002129  00000-0  69614-3 0  9997
2 40288  97.9762  34.6365 0156994 215.8819 143.1743 14.32685766620750

Epoch: 2026-10-10T12:51Z

TLE epoch observation values (Epoch: 2026-10-10T12:51:59.849Z)

Latitude

-0.00001°

Longitude

-177.5047°

Altitude

876.352 km

Speed

7.367 km/s

True Right ascension

02h 18m 32s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

23:47:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

892.251 km

Perigee altitude

667.498 km

Semi-major axis

7,158.011 km

Eccentricity

0.0157

Inclination

97.9762°

RAAN

34.6365°

Arg. of periapsis

215.8819°

True anomaly

144.23585°

Mean anomaly

143.1743°

Eccentric anomaly

143.70674°

Mean motion

3.58389 °/min

Orbital period

100.45 mins

BSTAR

0.00069614

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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.
4 mins	2026-10-11 05:49:25.621Z	79.88° E	2026-10-11 05:51:25.621Z	59.058° ENE	12.27°	2026-10-11 05:53:25.621Z	38.164° NE
10 mins	2026-10-11 07:25:25.621Z	161.275° S	2026-10-11 07:29:25.621Z	133.968° SE	74.159°	2026-10-11 07:35:25.621Z	349.614° N
4 mins	2026-10-11 09:08:25.621Z	255.634° W	2026-10-11 09:09:25.621Z	266.605° W	13.38°	2026-10-11 09:12:25.621Z	298.628° NW
7 mins	2026-10-11 19:39:25.621Z	44.385° NE	2026-10-11 19:42:25.621Z	96.153° ESE	31.16°	2026-10-11 19:46:25.621Z	156.044° SSE
7 mins	2026-10-11 21:18:25.621Z	342.855° N	2026-10-11 21:21:25.621Z	298.259° NW	28.163°	2026-10-11 21:25:25.621Z	237.584° WSW

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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, 40288

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-10-10T12:51:59.849Z)

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, 40288 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago