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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

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 (16 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: 4 days ago

TLE from 4 days ago

0 CZ-3B DEB
1 40167U 10042U   26232.42785837 -.00000081  00000-0  00000-0 0  9994
2 40167  26.7693 260.8732 7159641 349.9023   1.2757  1.93610817 96805

Epoch: 2026-08-20T10:16Z

TLE epoch observation values (Epoch: 2026-08-20T10:16:06.963Z)

Latitude

-0.0001°

Longitude

138.10942°

Altitude

1,413.872 km

Speed

9.362 km/s

True Right ascension

17h 23m 37s

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

00:46:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

40,288.888 km

Perigee altitude

1,346.448 km

Semi-major axis

27,195.805 km

Eccentricity

0.71596

Inclination

26.7693°

RAAN

260.8732°

Arg. of periapsis

349.9023°

True anomaly

10.98292°

Mean anomaly

1.2757°

Eccentric anomaly

4.47983°

Mean motion

0.48394 °/min

Orbital period

743.9 mins

BSTAR

0

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

CZ-3B DEB, 40160

CZ-3B DEB, 40815

CZ-3B DEB, 40158

CZ-3B DEB, 40163

CZ-3B DEB, 52965

CZ-3B DEB, 42458

CZ-3B DEB, 40165

CZ-3B DEB, 48542

CZ-3B DEB, 39333

CZ-3B DEB, 39337

CZ-3B DEB, 42459

CZ-3B DEB, 40166

CHINASAT 6A, 37150

CZ-3B DEB, 42465

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.
199 mins	2026-08-24 14:26:13.396Z	279.973° WNW	2026-08-24 15:32:13.396Z	267.422° W	20.275°	2026-08-24 17:45:13.396Z	267.019° W

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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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