CZ-2D DEB, 57730 (Decayed)
Orbit data source: Space-Track
CZ-2D DEB, 57730 was space debris in LEO originally from a launch on Thu, 31 Aug 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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57730 intel report (Beta)
CZ-2D DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 7 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 7 months ago
0 CZ-2D DEB
1 57730U 23130D 24150.55504847 .12114214 12436-5 14706-2 0 9998
2 57730 34.9658 104.6230 0010499 227.5015 286.6204 16.35014401 42032
Epoch: 2024-05-29T13:19Z
Definitive object data (Epoch: 2024-05-29T13:19:16.187Z)
Latitude | 14.59515° |
Longitude | 175.51603° |
Altitude | 175.252 km |
Speed | 7.806 km/s |
True Right ascension | 17h 31m 34s |
True Declination | 14° 30' 15" |
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 | 189.4 km |
Perigee altitude | 175.624 km |
Semi-major axis | 6,560.649 km |
Eccentricity | 0.0010499 |
Inclination | 34.9658° |
RAAN | 104.623° |
Arg. of periapsis | 227.5015° |
True anomaly | 286.50507° |
Mean anomaly | 286.6204° |
Eccentric anomaly | 286.56274° |
Mean motion | 4.08435 °/min |
BSTAR | 0.0014706 |
Orbital period | 88.14 mins |
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Other satellites on launch #130 in the year 2023 (2023-08-31 UTC)
YAOGAN-39 01A, 57727 |
YAOGAN-39 01B, 57728 |
CZ-2D R/B, 57729 (Decayed) |
CZ-2D DEB, 57730 (Decayed) |
YAOGAN-39 01C, 57731 |
CZ-2D DEB Visibility forecast
Observer location: undefined°, undefined
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