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 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 (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: 5 days ago

TLE from 5 days ago

0 CZ-3B DEB
1 40167U 10042U   25336.11187386 -.00000035  00000-0  00000-0 0  9998
2 40167  27.2348 321.9577 7160647 248.0140  25.9469  1.93642106 91748

Epoch: 2025-12-02T02:41Z

TLE epoch observation values (Epoch: 2025-12-02T02:41:05.901Z)

Latitude

-0.00019°

Longitude

-149.60051°

Altitude

11,657.43 km

Speed

5.435 km/s

True Right ascension

21h 27m 30s

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

06:25:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

40,286.52 km

Perigee altitude

1,342.868 km

Semi-major axis

27,192.831 km

Eccentricity

0.71606

Inclination

27.2348°

RAAN

321.9577°

Arg. of periapsis

248.014°

True anomaly

112.07771°

Mean anomaly

25.9469°

Eccentric anomaly

62.25858°

Mean motion

0.48402 °/min

Orbital period

743.77 mins

BSTAR

0

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

CZ-3B DEB, 40168

CZ-3B DEB, 42465

CZ-3B DEB, 42463

CZ-3B DEB, 40815

CZ-3B DEB, 39333

CZ-3B DEB, 39337

CZ-3B DEB, 40166

CZ-3B DEB, 39336

CZ-3B DEB, 39335

CZ-3B DEB, 48542

CZ-3B DEB, 40163

CZ-3B DEB, 40165

CZ-3B DEB, 42458

CZ-3B DEB, 40161

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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.
563 mins	2025-12-07 20:28:34.740Z	86.479° E	2025-12-08 03:45:34.740Z	106.654° ESE	39.292°	2025-12-08 05:51:34.740Z	103.907° ESE

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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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