CZ-3B DEB, 40167
Orbit data source: Space-Track
CZ-3B DEB, 40167 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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40167 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, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 CZ-3B DEB
1 40167U 10042U 25301.52874070 -.00000143 00000-0 00000-0 0 9998
2 40167 27.2881 330.2138 7166567 234.2787 36.7301 1.93653130 91077Epoch: 2025-10-28T12:41Z
TLE epoch observation values (Epoch: 2025-10-28T12:41:23.196Z)
Latitude
-0.00003°
Longitude
102.73051°
Altitude
16,307.695 km
Speed
4.525 km/s
True Right ascension
22h 00m 46s
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
04:05:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
40,300.852 km
Perigee altitude
1,326.478 km
Semi-major axis
27,191.802 km
Eccentricity
0.71666
Inclination
27.2881°
RAAN
330.2138°
Arg. of periapsis
234.2787°
True anomaly
125.62873°
Mean anomaly
36.7301°
Eccentric anomaly
76.68825°
Mean motion
0.48405 °/min
Orbital period
743.73 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. |
|---|---|---|---|---|---|---|---|
| 59 mins | 2025-11-10 07:46:42.874Z | 131.986° SE | 2025-11-10 07:46:42.874Z | 131.986° SE | 42.048° | 2025-11-10 08:45:42.874Z | 111.061° ESE |
| 565 mins | 2025-11-10 22:21:42.874Z | 142.786° SSE | 2025-11-11 07:08:42.874Z | 180.583° SSW | 43.962° | 2025-11-11 07:46:42.874Z | 183.27° SSW |
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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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 ascending order |
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