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.
Focus sentinelFocus sentinel
58142 intel report (Beta)
CZ-2D R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 1 month 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 | Payload Rocket body Debris |
Shape & HBR | Cyl + 1 Sail, 8.9 m |
Radar Cross Section | 27.824 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 1 month 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 54135
Epoch: 2024-10-08T12:38Z
Definitive object data (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 | Object was in full shadow at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 199.334 km |
Perigee altitude | 193.073 km |
Semi-major axis | 6,574.34 km |
Eccentricity | 0.0004762 |
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 |
BSTAR | 0.0023718 |
Orbital period | 88.42 mins |
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #163 in the year 2023 (2023-10-23 UTC)
YAOGAN-39 04A, 58141 |
CZ-2D R/B, 58142 (Decayed) |
YAOGAN-39 04B, 58143 |
CZ-2D DEB, 58144 (Decayed) |
YAOGAN-39 04C, 58145 |
CZ-2D R/B Visibility forecast
Observer location: undefined°, undefined
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. |
---|
Authenticating...
Click to sort rows by NORAD ID header in ascending order | Click to sort rows by Common name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|