CZ-3C DEB, 40832
Orbit data source: Space-Track
CZ-3C DEB, 40832 is space debris in HEO originally from a launch on Sun, 31 Oct 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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40832 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 10 months ago
TLE from 10 months ago
0 CZ-3C DEB
1 40832U 10057AZ 24307.18927890 .00000428 00000-0 37392-2 0 9990
2 40832 19.9495 238.7356 7172897 268.6665 16.1871 2.26618630 79802
Epoch: 2024-11-02T04:32Z
TLE epoch observation values (Epoch: 2024-11-02T04:32:33.696Z)
Latitude
0.00007°
Longitude
128.58711°
Altitude
5,724.723 km
Speed
7.042 km/s
True Right ascension
15h 54m 41s
True Declination
0° 00' 00"
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
16:50:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,674.489 km
Perigee altitude
544.813 km
Semi-major axis
24,487.788 km
Eccentricity
0.71729
Inclination
19.9495°
RAAN
238.7356°
Arg. of periapsis
268.6665°
True anomaly
91.8879°
Mean anomaly
16.1871°
Eccentric anomaly
45.50007°
Mean motion
0.56639 °/min
Orbital period
635.6 mins
BSTAR
0.0037392
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Other satellites on launch #57 in the year 2010 (2010-10-31 UTC)
CZ-3C 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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585 mins | 2025-08-31 07:10:51.884Z | 199.743° SSW | 2025-08-31 16:27:51.884Z | 177.929° S | 26.545° | 2025-08-31 16:55:51.884Z | 125.449° SE |
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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Authenticating...
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