CZ-3B DEB, 40169
Orbit data source: Space-Track
CZ-3B DEB, 40169 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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40169 intel report (Beta)
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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: 1 day ago
TLE from 1 day ago
0 CZ-3B DEB
1 40169U 10042W 26295.15767944 .00000086 00000-0 00000-0 0 9998
2 40169 25.6114 203.3419 7230064 92.1949 6.7641 1.93997703100260Epoch: 2026-10-22T03:47Z
TLE epoch observation values (Epoch: 2026-10-22T03:47:03.503Z)
Latitude
14.37533°
Longitude
-96.16111°
Altitude
2,667.409 km
Speed
8.571 km/s
True Right ascension
23h 24m 48s
True Declination
14° 18' 37"
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
04:53:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
40,418.491 km
Perigee altitude
1,144.973 km
Semi-major axis
27,159.869 km
Eccentricity
0.72301
Inclination
25.6114°
RAAN
203.3419°
Arg. of periapsis
92.1949°
True anomaly
53.5006°
Mean anomaly
6.7641°
Eccentric anomaly
22.85101°
Mean motion
0.4849 °/min
Orbital period
742.42 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. |
|---|---|---|---|---|---|---|---|
| 345 mins | 2026-10-23 10:23:32.098Z | 149.155° SSE | 2026-10-23 15:21:32.098Z | 164.175° S | 19.4° | 2026-10-23 16:08:32.098Z | 130.604° SE |
| 50 mins | 2026-10-24 05:13:32.098Z | 227.059° WSW | 2026-10-24 05:21:32.098Z | 185.302° SSW | 23.191° | 2026-10-24 06:03:32.098Z | 142.323° SSE |
| 13 mins | 2026-10-24 09:33:32.098Z | 149.484° SSE | 2026-10-24 09:46:32.098Z | 150.806° SSE | 10.65° | 2026-10-24 09:46:32.098Z | 150.806° SSE |
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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