CZ-2D R/B, 58142 (Decayed)
Orbit data source: Space-Track
CZ-2D R/B, 58142 was space debris in LEO originally from a launch on Mon, 23 Oct 2023 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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58142 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
BWYIC
Mission
Decayed spacecraft
Bus & Motor
CZ-2 STAGE 2, Unknown motor
Mass
4,006 kg wet, 4,006 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + 1 Sail, 4.5 m
Radar Cross Section
27.824 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 CZ-2D R/B
1 58142U 23163B 24282.52658632 .11432968 12836-5 23718-2 0 9992
2 58142 34.9547 199.7689 0004762 249.9087 287.0150 16.29904791 54135Epoch: 2024-10-08T12:38Z
TLE epoch observation values (Epoch: 2024-10-08T12:38:17.058Z)
Latitude
1.7598°
Longitude
170.05464°
Altitude
190.522 km
Speed
7.795 km/s
True Right ascension
01h 09m 03s
True Declination
1° 44' 54"
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
02:39:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
199.334 km
Perigee altitude
193.073 km
Semi-major axis
6,574.34 km
Eccentricity
0.00048
Inclination
34.9547°
RAAN
199.7689°
Arg. of periapsis
249.9087°
True anomaly
286.96281°
Mean anomaly
287.015°
Eccentric anomaly
286.98891°
Mean motion
4.0716 °/min
Orbital period
88.42 mins
BSTAR
0.0023718
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Other satellites on launch #163 in the year 2023 (2023-10-23 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-2D 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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