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
Last TLE update
9 months ago
Origin
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 & history
TLE from 9 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
No trajectory is available.
Visualization observer readout
No trajectory is available.
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)
CZ-2D R/B Visibility
Observer location: undefined°, undefined°
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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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Authenticating...
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