CZ-2D R/B, 57729 (Decayed)
Orbit data source: Space-Track
CZ-2D R/B, 57729 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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57729 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: 1 year ago
TLE from 1 year ago
0 CZ-2D R/B
1 57729U 23130C 24175.13562002 .29124601 14075-5 29545-2 0 9991
2 57729 34.9650 308.9663 0007021 338.7115 196.8926 16.36759841 45798Epoch: 2024-06-23T03:15Z
TLE epoch observation values (Epoch: 2024-06-23T03:15:17.569Z)
Latitude
2.50341°
Longitude
164.79028°
Altitude
177.397 km
Speed
7.8 km/s
True Right ascension
08h 21m 36s
True Declination
2° 29' 14"
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
05:58:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
182.455 km
Perigee altitude
173.249 km
Semi-major axis
6,555.989 km
Eccentricity
0.0007
Inclination
34.965°
RAAN
308.9663°
Arg. of periapsis
338.7115°
True anomaly
196.86924°
Mean anomaly
196.8926°
Eccentric anomaly
196.88092°
Mean motion
4.08871 °/min
Orbital period
88.05 mins
BSTAR
0.0029545
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Other satellites on launch #130 in the year 2023 (2023-08-31 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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