CZ-2D DEB, 35272

Orbit data source: Space-Track

CZ-2D DEB, 35272 is space debris in SSO originally from a launch on Tue, 05 Jul 2005 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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/35272?theme=dark&initialShowStats=false

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Identifier

35272, 2005-024L

Orbit

SSO

Country

CN / PRC

Related business

China Aerospace Science and Technology Corporation (CASC) (CN)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

2005-07-05 (20 years ago)

Launch vehicle

Unknown

Launch site

Jiuquan Satellite Launch Center, China (JSC)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago

0 CZ-2D DEB
1 35272U 05024L   25351.31765940  .00046088  00000-0  44385-3 0  9994
2 35272  97.1853  18.0005 0006954  84.0348 276.1705 15.66381603110772

Epoch: 2025-12-17T07:37Z

TLE epoch observation values (Epoch: 2025-12-17T07:37:25.772Z)

Latitude

-0.00002°

Longitude

177.45387°

Altitude

371.926 km

Speed

7.687 km/s

True Right ascension

01h 12m 00s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

13:44:03

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

370.853 km

Perigee altitude

361.473 km

Semi-major axis

6,744.3 km

Eccentricity

0.0007

Inclination

97.1853°

RAAN

18.0005°

Arg. of periapsis

84.0348°

True anomaly

276.09127°

Mean anomaly

276.1705°

Eccentric anomaly

276.13088°

Mean motion

3.91866 °/min

Orbital period

91.87 mins

BSTAR

0.00044385

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Other satellites on launch #24 in the year 2005 (2005-07-05 UTC)

SJ-7, 28737

CZ-2D R/B, 28738

CZ-2D DEB, 35271

CZ-2D DEB, 28785 (Decayed)

CZ-2D DEB, 31409

CZ-2D DEB, 28739 (Decayed)

CZ-2D DEB, 35273

CZ-2D DEB, 28742 (Decayed)

CZ-2D DEB, 29217 (Decayed)

SJ-7 DEB, 44901 (Decayed)

CZ-2D DEB, 28740 (Decayed)

CZ-2D DEB, 28741 (Decayed)

SJ-7 DEB, 44902 (Decayed)

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CZ-2D 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.
4 mins	2025-12-20 01:41:41.993Z	133.073° SE	2025-12-20 01:43:41.993Z	52.869° ENE	29.976°	2025-12-20 01:45:41.993Z	7.089° NNE

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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-2D DEB, 35272 on other resources

View CZ-2D DEB, 35272 on Heavens-Above

View CZ-2D DEB, 35272 on Keep Track

View CZ-2D DEB, 35272 on Celestrak

View CZ-2D DEB, 35272 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-2D DEB, 35272

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2025-12-17T07:37:25.772Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #24 in the year 2005 (2005-07-05 UTC)

CZ-2D DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out CZ-2D DEB, 35272 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago