CZ-2D R/B, 59558 (Decayed)
Orbit data source: Space-Track
CZ-2D R/B, 59558 was space debris in LEO originally from a launch on Sat, 20 Apr 2024 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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59558 intel report (Beta)
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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, 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 59558U 24075B 25142.21743938 .05071819 14054-5 60636-3 0 9995
2 59558 35.0616 83.2271 0005409 225.9538 273.2258 16.35318442 61755Epoch: 2025-05-22T05:13Z
TLE epoch observation values (Epoch: 2025-05-22T05:13:06.762Z)
Latitude
22.17843°
Longitude
-90.41746°
Altitude
176.696 km
Speed
7.805 km/s
True Right ascension
15h 11m 48s
True Declination
22° 02' 52"
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
23:07:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
185.232 km
Perigee altitude
178.135 km
Semi-major axis
6,559.82 km
Eccentricity
0.00054
Inclination
35.0616°
RAAN
83.2271°
Arg. of periapsis
225.9538°
True anomaly
273.16391°
Mean anomaly
273.2258°
Eccentric anomaly
273.19486°
Mean motion
4.08512 °/min
Orbital period
88.12 mins
BSTAR
0.00060636
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Other satellites on launch #75 in the year 2024 (2024-04-20 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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