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: 2 days ago

TLE from 2 days ago

0 CZ-3C DEB (VEB)
1 38095U 12008C   25337.97108749  .00010015  00000-0  23465-2 0  9990
2 38095  20.8432 123.6966 6576002 223.5976  59.9638  3.20876242133594

Epoch: 2025-12-03T23:18Z

TLE epoch observation values (Epoch: 2025-12-03T23:18:21.959Z)

Latitude

-0.00014°

Longitude

60.97774°

Altitude

14,651.02 km

Speed

4.169 km/s

True Right ascension

08h 14m 24s

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

05:10:29

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

25,814.235 km

Perigee altitude

271.634 km

Semi-major axis

19,421.072 km

Eccentricity

0.6576

Inclination

20.8432°

RAAN

123.6966°

Arg. of periapsis

223.5976°

True anomaly

136.42185°

Mean anomaly

59.9638°

Eccentric anomaly

97.33333°

Mean motion

0.80192 °/min

Orbital period

448.92 mins

BSTAR

0.0023465

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

CZ-3C DEB, 40860

CZ-3C DEB, 40194

CZ-3C DEB, 40868

CZ-3C DEB, 42478

BEIDOU 11, 38091

CZ-3C DEB, 40854

CZ-3C DEB, 40196

CZ-3C DEB, 40866

CZ-3C DEB, 40206

CZ-3C DEB, 40863

CZ-3C DEB, 48550

CZ-3C DEB, 40197

CZ-3C DEB, 40856

CZ-3C DEB, 40858

CZ-3C DEB, 42480

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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-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.
383 mins	2025-12-06 10:34:39.418Z	214.468° SW	2025-12-06 15:54:39.418Z	189.761° SSW	41.818°	2025-12-06 16:57:39.418Z	117.905° 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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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.

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