CZ-3B DEB, 39334

Orbit data source: Space-Track

CZ-3B DEB, 39334 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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Iframe URL

https://www.satcat.com/sats-embedded/39334?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39334, 2010-042F

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: 6 hours ago

TLE from 6 hours ago

0 CZ-3B DEB
1 39334U 10042F   25342.60081087 -.00000226  00000-0  00000-0 0  9996
2 39334  26.5450 286.1933 7344319 327.6864 287.0240  1.86384577 94268

Epoch: 2025-12-08T14:25Z

TLE epoch observation values (Epoch: 2025-12-08T14:25:10.059Z)

Latitude

1.2318°

Longitude

169.77399°

Altitude

29,211.922 km

Speed

2.847 km/s

True Right ascension

06h 54m 39s

True Declination

1° 13' 49"

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

18:40:27

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

42,002.822 km

Perigee altitude

1,029.729 km

Semi-major axis

27,894.412 km

Eccentricity

0.73443

Inclination

26.545°

RAAN

286.1933°

Arg. of periapsis

327.6864°

True anomaly

209.57382°

Mean anomaly

287.024°

Eccentric anomaly

248.00647°

Mean motion

0.46587 °/min

Orbital period

772.74 mins

BSTAR

0

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Other satellites on launch #42 in the year 2010 (2010-09-04 UTC)

CZ-3B DEB, 40168

CZ-3B DEB, 42463

CZ-3B DEB, 40158

CZ-3B DEB, 40159

CZ-3B DEB, 40161

CZ-3B DEB, 39336

CZ-3B DEB, 40162

CZ-3B DEB, 40169

CZ-3B DEB, 39335

CZ-3B DEB, 40163

CZ-3B DEB, 42464

CZ-3B DEB, 42459

CZ-3B DEB, 40164

CZ-3B DEB, 40160

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.

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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.
317 mins	2025-12-09 06:44:32.586Z	279.438° WNW	2025-12-09 08:14:32.586Z	266.815° W	29.065°	2025-12-09 12:01:32.586Z	274.284° 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, 39334 on other resources

View CZ-3B DEB, 39334 on Heavens-Above

View CZ-3B DEB, 39334 on Keep Track

View CZ-3B DEB, 39334 on Celestrak

View CZ-3B DEB, 39334 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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