CZ-3C DEB, 40856
Orbit data source: Space-Track
CZ-3C DEB, 40856 is space debris in HEO originally from a launch on Fri, 24 Feb 2012 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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40856 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CZ-3C DEB
1 40856U 12008W 25293.43858425 -.00000150 00000-0 10776-2 0 9994
2 40856 21.9617 4.3079 7061995 195.4446 119.7793 2.35428364 93550Epoch: 2025-10-20T10:31Z
TLE epoch observation values (Epoch: 2025-10-20T10:31:33.679Z)
Latitude
0.00002°
Longitude
177.27261°
Altitude
31,098.277 km
Speed
2.138 km/s
True Right ascension
00h 17m 12s
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
06:02:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,353.714 km
Perigee altitude
635.719 km
Semi-major axis
23,872.854 km
Eccentricity
0.7062
Inclination
21.9617°
RAAN
4.3079°
Arg. of periapsis
195.4446°
True anomaly
164.51657°
Mean anomaly
119.7793°
Eccentric anomaly
143.72134°
Mean motion
0.58842 °/min
Orbital period
611.81 mins
BSTAR
0.0010776
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Other satellites on launch #8 in the year 2012 (2012-02-24 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-3C 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. |
|---|---|---|---|---|---|---|---|
| 147 mins | 2025-10-21 11:02:41.131Z | 253.15° W | 2025-10-21 13:15:41.131Z | 212.543° SW | 36.101° | 2025-10-21 13:29:41.131Z | 143.356° SSE |
| 532 mins | 2025-10-22 00:49:41.131Z | 153.22° SSE | 2025-10-22 08:36:41.131Z | 164.498° S | 41.213° | 2025-10-22 09:41:41.131Z | 102.832° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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