CZ-2C R/B, 46811 (Decayed)
Orbit data source: Space-Track
CZ-2C R/B, 46811 was space debris in LEO originally from a launch on Mon, 26 Oct 2020 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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46811 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CALT
Mission
Decayed spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
~3,800 kg wet, ~3,800 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 3.7 m
Radar Cross Section
23.715 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 CZ-2C R/B
1 46811U 20076E 25013.97453432 .06011521 18079-5 50991-3 0 9996
2 46811 35.2897 211.7451 0009288 302.7058 181.9249 16.38235214235974Epoch: 2025-01-13T23:23Z
TLE epoch observation values (Epoch: 2025-01-13T23:23:19.765Z)
Latitude
28.50982°
Longitude
-122.50781°
Altitude
175.997 km
Speed
7.802 km/s
True Right ascension
22h 48m 02s
True Declination
28° 21' 11"
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
17:51:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
179.951 km
Perigee altitude
167.78 km
Semi-major axis
6,552.002 km
Eccentricity
0.00093
Inclination
35.2897°
RAAN
211.7451°
Arg. of periapsis
302.7058°
True anomaly
181.92133°
Mean anomaly
181.9249°
Eccentric anomaly
181.92311°
Mean motion
4.09244 °/min
Orbital period
87.97 mins
BSTAR
0.00050991
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Other satellites on launch #76 in the year 2020 (2020-10-26 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-2C R/B 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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