CZ-4B DEB, 46480 (Decayed)
Orbit data source: Space-Track
CZ-4B DEB, 46480 was space debris in LEO originally from a launch on Sun, 27 Sep 2020 UTC launched from the Taiyaun Space Center, China (TSC). 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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46480 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SAST
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 2.7 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 CZ-4B DEB
1 46480U 20067C 26222.33903981 .11965540 28380-5 94818-3 0 9997
2 46480 97.8608 1.2426 0016933 274.7833 85.1530 16.38948308321023Epoch: 2026-08-10T08:08Z
TLE epoch observation values (Epoch: 2026-08-10T08:08:13.039Z)
Latitude
-0.00011°
Longitude
-79.63482°
Altitude
170.919 km
Speed
7.804 km/s
True Right ascension
00h 04m 58s
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
09:20:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
176.512 km
Perigee altitude
154.352 km
Semi-major axis
6,543.569 km
Eccentricity
0.00169
Inclination
97.8608°
RAAN
1.2426°
Arg. of periapsis
274.7833°
True anomaly
85.34638°
Mean anomaly
85.153°
Eccentric anomaly
85.24969°
Mean motion
4.10035 °/min
Orbital period
87.8 mins
BSTAR
0.00094818
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Other satellites on launch #67 in the year 2020 (2020-09-27 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
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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. |
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| This satellite is decayed. |
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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