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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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ISO8601 Format

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: 15 hours ago

TLE from 15 hours ago

0 CZ-3C DEB (VEB)
1 38095U 12008C   26046.01342553  .00014479  00000-0  17949-2 0  9994
2 38095  20.8756  80.3458 6581763 301.5238  10.4508  3.22439853135940

Epoch: 2026-02-15T00:19Z

TLE epoch observation values (Epoch: 2026-02-15T00:19:19.965Z)

Latitude

-0.00003°

Longitude

-69.45595°

Altitude

1,799.943 km

Speed

8.768 km/s

True Right ascension

05h 21m 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

17:51:00

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

25,721.285 km

Perigee altitude

238.978 km

Semi-major axis

19,358.268 km

Eccentricity

0.65818

Inclination

20.8756°

RAAN

80.3458°

Arg. of periapsis

301.5238°

True anomaly

58.20774°

Mean anomaly

10.4508°

Eccentric anomaly

28.36896°

Mean motion

0.80583 °/min

Orbital period

446.74 mins

BSTAR

0.0017949

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

CZ-3C DEB, 48549

CZ-3C DEB, 42477

CZ-3C DEB, 40855

CZ-3C DEB, 40869

CZ-3C DEB, 42478

CZ-3C R/B, 38092 (Decayed)

CZ-3C DEB, 40862

CZ-3C DEB, 40197

CZ-3C DEB, 40199

CZ-3C DEB, 40867

CZ-3C DEB, 40863

CZ-3C DEB, 40866

CZ-3C DEB, 40854

CZ-3C DEB, 40200

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-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.
381 mins	2026-02-16 06:14:55.476Z	229.313° WSW	2026-02-16 07:06:55.476Z	152.682° SSE	40.88°	2026-02-16 12:35:55.476Z	132.268° SE

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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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Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in descending order

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.

Documentation

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