CZ-3B DEB, 40160
Orbit data source: Space-Track
CZ-3B DEB, 40160 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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40160 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, 0.3 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 CZ-3B DEB
1 40160U 10042M 25329.75867145 -.00000063 00000-0 00000-0 0 9992
2 40160 27.2897 304.8870 7260305 269.7648 245.1221 1.89921954 83357Epoch: 2025-11-25T18:12Z
TLE epoch observation values (Epoch: 2025-11-25T18:12:29.213Z)
Latitude
26.18382°
Longitude
74.50482°
Altitude
36,751.271 km
Speed
2.003 km/s
True Right ascension
03h 30m 15s
True Declination
26° 09' 41"
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
20:41:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
41,168.545 km
Perigee altitude
1,168.856 km
Semi-major axis
27,546.838 km
Eccentricity
0.72603
Inclination
27.2897°
RAAN
304.887°
Arg. of periapsis
269.7648°
True anomaly
196.04503°
Mean anomaly
245.1221°
Eccentric anomaly
218.96377°
Mean motion
0.47472 °/min
Orbital period
758.35 mins
BSTAR
0
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Other satellites on launch #42 in the year 2010 (2010-09-04 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 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. |
|---|---|---|---|---|---|---|---|
| 220 mins | 2025-11-30 23:19:50.757Z | 69.489° E | 2025-12-01 01:39:50.757Z | 80.212° E | 16.684° | 2025-12-01 02:59:50.757Z | 85.601° E |
| 255 mins | 2025-12-01 06:04:50.757Z | 273.894° WNW | 2025-12-01 07:33:50.757Z | 279.132° WNW | 18.973° | 2025-12-01 10:19:50.757Z | 291.005° WNW |
| 62 mins | 2025-12-01 21:59:50.757Z | 69.665° E | 2025-12-01 23:01:50.757Z | 73.565° E | 15.844° | 2025-12-01 23:01:50.757Z | 73.565° E |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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