CZ-4B DEB, 40532
Orbit data source: Space-Track
CZ-4B DEB, 40532 is space debris in LEO originally from a launch on Fri, 25 Oct 2013 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). 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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40532 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 CZ-4B DEB
1 40532U 13057E 25305.81715272 .00004030 00000-0 74906-3 0 9994
2 40532 74.8681 244.6453 0185757 118.5757 243.4246 14.54824870558405Epoch: 2025-11-01T19:36Z
TLE epoch observation values (Epoch: 2025-11-01T19:36:41.995Z)
Latitude
0.00008°
Longitude
-90.87145°
Altitude
773.463 km
Speed
7.435 km/s
True Right ascension
16h 18m 34s
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
17:54:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
839.086 km
Perigee altitude
575.846 km
Semi-major axis
7,085.603 km
Eccentricity
0.01858
Inclination
74.8681°
RAAN
244.6453°
Arg. of periapsis
118.5757°
True anomaly
241.5408°
Mean anomaly
243.4246°
Eccentric anomaly
242.48071°
Mean motion
3.63897 °/min
Orbital period
98.93 mins
BSTAR
0.00074906
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Other satellites on launch #57 in the year 2013 (2013-10-25 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-4B 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-04 07:36:49.336Z | 318.364° NNW | 2025-11-04 07:38:49.336Z | 270.798° WNW | 34.909° | 2025-11-04 07:42:49.336Z | 185.993° SSW |
| 7 mins | 2025-11-04 20:21:49.336Z | 167.7° S | 2025-11-04 20:24:49.336Z | 102.079° ESE | 35.826° | 2025-11-04 20:28:49.336Z | 31.744° NE |
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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