JIELONG 3 DEB, 58506 (Decayed)
Orbit data source: Space-Track
JIELONG 3 DEB, 58506 was space debris in LEO originally from a launch on Tue, 05 Dec 2023 UTC launched from the South China Sea Launch Area (SCSLA). 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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58506 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changzheng H.
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 months ago
TLE from 11 months ago
0 JIELONG 3 DEB
1 58506U 23190B 25188.06370650 .06177803 -14875-5 11426-2 0 9999
2 58506 86.5212 35.6777 0011788 354.9804 5.1379 16.32147798 87708Epoch: 2025-07-07T01:31Z
TLE epoch observation values (Epoch: 2025-07-07T01:31:44.241Z)
Latitude
-0.00006°
Longitude
87.46494°
Altitude
182.392 km
Speed
7.801 km/s
True Right ascension
02h 22m 42s
True Declination
0° 00' 00"
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
13:09:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
191.197 km
Perigee altitude
175.727 km
Semi-major axis
6,561.599 km
Eccentricity
0.00118
Inclination
86.5212°
RAAN
35.6777°
Arg. of periapsis
354.9804°
True anomaly
5.15001°
Mean anomaly
5.1379°
Eccentric anomaly
5.14396°
Mean motion
4.08346 °/min
Orbital period
88.16 mins
BSTAR
0.0011426
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Other satellites on launch #190 in the year 2023 (2023-12-05 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.JIELONG 3 DEB 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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