CZ-3B DEB, 39337

Orbit data source: Space-Track

CZ-3B DEB, 39337 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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https://www.satcat.com/sats-embedded/39337?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39337, 2010-042J

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, 0.3 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 CZ-3B DEB
1 39337U 10042J   25337.85829941  .00000088  00000-0  20930-2 0  9990
2 39337  24.4164 168.3945 7463969 203.6458  86.2864  1.84157471 79105

Epoch: 2025-12-03T20:35Z

TLE epoch observation values (Epoch: 2025-12-03T20:35:57.069Z)

Latitude

-0.00035°

Longitude

146.41399°

Altitude

32,912.139 km

Speed

2.472 km/s

True Right ascension

11h 13m 17s

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

06:26:58

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

42,729.219 km

Perigee altitude

752.99 km

Semi-major axis

28,119.241 km

Eccentricity

0.7464

Inclination

24.4164°

RAAN

168.3945°

Arg. of periapsis

203.6458°

True anomaly

156.33392°

Mean anomaly

86.2864°

Eccentric anomaly

122.39601°

Mean motion

0.4603 °/min

Orbital period

782.1 mins

BSTAR

0.002093

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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, 40167

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.
372 mins	2025-12-07 13:51:59.313Z	224.005° SW	2025-12-07 15:55:59.313Z	234.214° WSW	25.379°	2025-12-07 20:03:59.313Z	271.247° WNW

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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, 39337 on other resources

View CZ-3B DEB, 39337 on Heavens-Above

View CZ-3B DEB, 39337 on Keep Track

View CZ-3B DEB, 39337 on Celestrak

View CZ-3B DEB, 39337 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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