CZ-2D DEB, 58144 (Decayed)
Orbit data source: Space-Track
CZ-2D DEB, 58144 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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58144 intel report (Beta)
CZ-2D DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 5 months ago |
Origin | |
Manufacturer | SAST |
Mission | Decayed spacecraft |
Bus & Motor | Unknown |
Mass | 300 kg wet, 300 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cone + 1 Sail, 5 m |
Radar Cross Section | 4.639 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 5 months ago
0 CZ-2D DEB
1 58144U 23163D 24204.77725051 .08939502 14539-5 22271-2 0 9992
2 58144 34.9775 336.7201 0010539 348.7546 128.8930 16.27794060 42195
Epoch: 2024-07-22T18:39Z
Definitive object data (Epoch: 2024-07-22T18:39:14.444Z)
Latitude | 30.62413° |
Longitude | -121.37024° |
Altitude | 202.552 km |
Speed | 7.788 km/s |
True Right ascension | 06h 37m 46s |
True Declination | 30° 27' 39" |
Sunlit | Object was in daylight 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 | 208.81 km |
Perigee altitude | 194.941 km |
Semi-major axis | 6,580.013 km |
Eccentricity | 0.0010539 |
Inclination | 34.9775° |
RAAN | 336.7201° |
Arg. of periapsis | 348.7546° |
True anomaly | 128.98692° |
Mean anomaly | 128.893° |
Eccentric anomaly | 128.93997° |
Mean motion | 4.06633 °/min |
BSTAR | 0.0022271 |
Orbital period | 88.53 mins |
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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 DEB Visibility forecast
Observer location: undefined°, undefined
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