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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39333 intel report (Beta)
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Edit Public Description
Expand to show TLE details & history
TLE from 2 days ago
0 CZ-3B DEB
1 39333U 10042E 25198.32080131 .00000217 00000-0 16735-2 0 9995
2 39333 23.6512 112.2789 7485859 332.9081 292.1589 1.91221314 83702
Epoch: 2025-07-17T07:41Z
TLE epoch observation values (Epoch: 2025-07-17T07:41:57.233Z)
Latitude
-1.40917°
Longitude
-115.46097°
Altitude
27,593.578 km
Speed
2.988 km/s
True Right ascension
19h 41m 39s
True Declination
-1° 24' 27"
Sunlit
Visualization orbit readout
Latitude
-16.22973°
Longitude
19.6436°
Altitude
649.312 km
Speed
9.946 km/s
Apparent Right ascension
02h 57m 15s
Apparent Declination
-31° 12' 29"
Sunlit
Visualization observer readout
Local Sidereal Time
12:27:20
Azimuth
274.191° WNW
Elevation
-58.548°
Doppler factor
1
Orbital elements
Apogee altitude
41,572.874 km
Perigee altitude
516.326 km
Semi-major axis
27,422.737 km
Eccentricity
0.74859
Inclination
23.6512°
RAAN
112.2789°
Arg. of periapsis
332.9081°
True anomaly
210.52988°
Mean anomaly
292.1589°
Eccentric anomaly
251.4875°
Mean motion
0.47794 °/min
Orbital period
753.23 mins
BSTAR
0.0016735
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Other satellites on launch #42 in the year 2010 (2010-09-04 UTC)
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. |
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661 mins | 2025-07-19 00:01:41.969Z | 245.351° WSW | 2025-07-19 00:39:41.969Z | 167.7° S | 42.312° | 2025-07-19 11:02:41.969Z | 228.836° WSW |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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