CZ-3B DEB, 40185
Orbit data source: Space-Track
CZ-3B DEB, 40185 is space debris in HEO originally from a launch on Mon, 19 Dec 2011 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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40185 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 CZ-3B DEB
1 40185U 11077J 25259.42488000 -.00000073 00000-0 70303-3 0 9990
2 40185 25.9456 319.4892 7469849 125.0160 328.4277 1.92817059 80046
Epoch: 2025-09-16T10:11Z
TLE epoch observation values (Epoch: 2025-09-16T10:11:49.631Z)
Latitude
0.00034°
Longitude
170.99435°
Altitude
14,738.198 km
Speed
4.81 km/s
True Right ascension
21h 18m 15s
True Declination
0° 00' 01"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
18:07:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
41,263.868 km
Perigee altitude
521.835 km
Semi-major axis
27,270.988 km
Eccentricity
0.74698
Inclination
25.9456°
RAAN
319.4892°
Arg. of periapsis
125.016°
True anomaly
234.98223°
Mean anomaly
328.4277°
Eccentric anomaly
287.64137°
Mean motion
0.48194 °/min
Orbital period
746.98 mins
BSTAR
0.00070303
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Other satellites on launch #77 in the year 2011 (2011-12-19 UTC)
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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.CZ-3B DEB Visibility
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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. |
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CZ-3B DEB is likely not visible in the next few days. |
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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