CZ-3B DEB, 40182

Orbit data source: Space-Track

CZ-3B DEB, 40182 is space debris in HEO originally from a launch on Mon, 19 Dec 2011 UTC launched from the Xichang Space Center, China (XSC). 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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Iframe URL

https://www.satcat.com/sats-embedded/40182?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40182, 2011-077F

Orbit

HEO

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

Manufacturer

CALT

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2011-12-19 (14 years ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.2 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 week ago

TLE from 1 week ago

0 CZ-3B DEB
1 40182U 11077F   25331.95584007 -.00000129  00000-0 -10319-2 0  9993
2 40182  23.1163 320.7844 7523816 204.7539  82.1040  1.87698087 81203

Epoch: 2025-11-27T22:56Z

TLE epoch observation values (Epoch: 2025-11-27T22:56:24.582Z)

Latitude

-0.00015°

Longitude

-90.44809°

Altitude

31,639.685 km

Speed

2.571 km/s

True Right ascension

21h 23m 02s

True Declination

0° 00' 01"

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

11:58:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

42,276.509 km

Perigee altitude

496.956 km

Semi-major axis

27,764.869 km

Eccentricity

0.75238

Inclination

23.1163°

RAAN

320.7844°

Arg. of periapsis

204.7539°

True anomaly

155.31364°

Mean anomaly

82.104°

Eccentric anomaly

119.59011°

Mean motion

0.46914 °/min

Orbital period

767.37 mins

BSTAR

-0.0010319

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Other satellites on launch #77 in the year 2011 (2011-12-19 UTC)

CZ-3B DEB, 40847

CZ-3B DEB, 40191

CZ-3B DEB, 40186

CZ-3B DEB, 40192

CZ-3B DEB, 40180

CZ-3B R/B, 38015 (Decayed)

CZ-3B DEB, 41120

CZ-3B DEB, 40846

CZ-3B DEB, 48546

CZ-3B DEB, 40845

CZ-3B DEB, 40843

CZ-3B DEB, 40851

CZ-3B DEB, 40187

CZ-3B DEB, 40840

CZ-3B DEB, 40842

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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CZ-3B 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.
713 mins	2025-12-05 20:30:23.010Z	181.048° SSW	2025-12-06 01:23:23.010Z	199.417° SSW	38.719°	2025-12-06 08:23:23.010Z	149.778° SSE

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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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Check out CZ-3B DEB, 40182 on other resources

View CZ-3B DEB, 40182 on Heavens-Above

View CZ-3B DEB, 40182 on Keep Track

View CZ-3B DEB, 40182 on Celestrak

View CZ-3B DEB, 40182 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

Documentation

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