CZ-3C DEB (VEB), 38095

Orbit data source: Space-Track

CZ-3C DEB (VEB), 38095 is space debris in HEO originally from a launch on Fri, 24 Feb 2012 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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https://www.satcat.com/sats-embedded/38095?theme=dark&initialShowStats=false

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Identifier

38095, 2012-008C

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)

2012-02-24 (14 years ago)

Launch vehicle

Unknown

Launch site

Xichang Space Center, China (XSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.5 m

Radar Cross Section

5.890 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 CZ-3C DEB (VEB)
1 38095U 12008C   26120.03397449  .00036968  00000-0  31389-2 0  9994
2 38095  21.0145  35.6408 6562347  21.9513 356.4083  3.26351987138342

Epoch: 2026-04-30T00:48Z

TLE epoch observation values (Epoch: 2026-04-30T00:48:55.395Z)

Latitude

-0.00019°

Longitude

165.40953°

Altitude

401.13 km

Speed

9.84 km/s

True Right ascension

02h 22m 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

20:14:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

25,427.003 km

Perigee altitude

223.284 km

Semi-major axis

19,203.28 km

Eccentricity

0.65623

Inclination

21.0145°

RAAN

35.6408°

Arg. of periapsis

21.9513°

True anomaly

337.53209°

Mean anomaly

356.4083°

Eccentric anomaly

349.65889°

Mean motion

0.81561 °/min

Orbital period

441.39 mins

BSTAR

0.0031389

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Other satellites on launch #8 in the year 2012 (2012-02-24 UTC)

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CZ-3C DEB (VEB) 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.
17 mins	2026-04-30 23:05:57.572Z	178.804° S	2026-04-30 23:09:57.572Z	140.884° SSE	18.376°	2026-04-30 23:22:57.572Z	103.408° ESE
332 mins	2026-05-01 06:53:57.572Z	256.482° W	2026-05-01 07:57:57.572Z	220.414° SW	28.838°	2026-05-01 12:25:57.572Z	201.549° SSW

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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-3C DEB (VEB), 38095 on other resources

View CZ-3C DEB (VEB), 38095 on Heavens-Above

View CZ-3C DEB (VEB), 38095 on Keep Track

View CZ-3C DEB (VEB), 38095 on Celestrak

View CZ-3C DEB (VEB), 38095 on Gunter's Space Page

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

CZ-3C DEB (VEB), 38095

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-04-30T00:48:55.395Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #8 in the year 2012 (2012-02-24 UTC)

CZ-3C DEB (VEB) Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-3C DEB (VEB), 38095 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago