CZ-3B DEB, 39333

Orbit data source: Space-Track

CZ-3B DEB, 39333 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/39333?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39333, 2010-042E

Orbit

HEO

Last TLE update

10 hours ago

Origin

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

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

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 10 hours ago

0 CZ-3B DEB
1 39333U 10042E   25188.92915483  .00000437  00000-0  39218-2 0  9992
2 39333  23.5969 115.0923 7489330 328.1011 306.9769  1.91217678 83528

Epoch: 2025-07-07T22:17Z

TLE epoch observation values (Epoch: 2025-07-07T22:17:58.977Z)

Latitude

-2.39838°

Longitude

39.84035°

Altitude

23,129.619 km

Speed

3.532 km/s

True Right ascension

20h 01m 52s

True Declination

-2° 23' 42"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

7.16143°

Longitude

17.5793°

Altitude

37,959.575 km

Speed

1.855 km/s

Apparent Right ascension

18h 18m 31s

Apparent Declination

2° 05' 09"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

20:34:41

Azimuth

228.014° WSW

Elevation

41.185°

Doppler factor

Orbital elements

Apogee altitude

41,583.023 km

Perigee altitude

506.898 km

Semi-major axis

27,423.097 km

Eccentricity

0.74893

Inclination

23.5969°

RAAN

115.0923°

Arg. of periapsis

328.1011°

True anomaly

Unknown

Mean anomaly

306.9769°

Eccentric anomaly

Unknown

Mean motion

0.47793 °/min

Orbital period

753.24 mins

BSTAR

0.0039218

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

CZ-3B R/B, 37151 (Decayed)

CZ-3B DEB Visibility forecast

Observer location: undefined°, undefined°

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.
194 mins	2025-07-08 08:28:58.042Z	227.999° WSW	2025-07-08 08:28:58.042Z	227.999° WSW	33.358°	2025-07-08 11:42:58.042Z	223.099° SW
410 mins	2025-07-09 01:38:58.042Z	252.05° W	2025-07-09 02:52:58.042Z	186.53° SSW	42.716°	2025-07-09 08:28:58.042Z	239.028° WSW

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Check out CZ-3B DEB, 39333 on other resources

View CZ-3B DEB, 39333 on Heavens-Above

View CZ-3B DEB, 39333 on Keep Track

View CZ-3B DEB, 39333 on Celestrak

View CZ-3B DEB, 39333 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.