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CZ-3B DEB, 40167

Orbit data source: Space-Track

CZ-3B DEB, 40167 is space debris in HEO originally from a launch on Sat, 04 Sep 2010 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 src="https://www.satcat.com/sats-embedded/40167?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/40167?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

40167, 2010-042U

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)

2010-09-04 (15 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: 2 weeks ago

TLE from 2 weeks ago

0 CZ-3B DEB
1 40167U 10042U   26012.93344514  .00000256  00000-0  00000+0 0  9991
2 40167  27.1871 312.0937 7150150 264.3936  17.9917  1.93614543 92554

Epoch: 2026-01-12T22:24Z

TLE epoch observation values (Epoch: 2026-01-12T22:24:09.660Z)

Latitude

0.00016°

Longitude

-136.36773°

Altitude

7,937.841 km

Speed

6.405 km/s

True Right ascension

20h 48m 22s

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

12:57:31

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

40,262.383 km

Perigee altitude

1,372.144 km

Semi-major axis

27,195.4 km

Eccentricity

0.71502

Inclination

27.1871°

RAAN

312.0937°

Arg. of periapsis

264.3936°

True anomaly

96.15216°

Mean anomaly

17.9917°

Eccentric anomaly

48.8305°

Mean motion

0.48395 °/min

Orbital period

743.88 mins

BSTAR

0

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Other satellites on launch #42 in the year 2010 (2010-09-04 UTC)

CHINASAT 6A, 37150

CZ-3B DEB, 40160

CZ-3B DEB, 40162

CZ-3B DEB, 40169

CZ-3B DEB, 39334

CZ-3B DEB, 42459

CZ-3B DEB, 40164

CZ-3B DEB, 42464

CZ-3B R/B, 37151 (Decayed)

CZ-3B DEB, 39332

CZ-3B DEB, 42460

CZ-3B DEB, 40814

CZ-3B DEB, 42458

CZ-3B DEB, 40166

Did you know?

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

Click here to try in Sandbox

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.
681 mins	2026-01-27 21:49:57.670Z	232.364° WSW	2026-01-28 00:25:57.670Z	226.746° WSW	42.358°	2026-01-28 09:10:57.670Z	215.155° SW

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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, 40167 on other resources

View CZ-3B DEB, 40167 on Heavens-Above

View CZ-3B DEB, 40167 on Keep Track

View CZ-3B DEB, 40167 on Celestrak

View CZ-3B DEB, 40167 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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