JIELONG 3 R/B, 65562 (Decayed)
Orbit data source: Space-Track
JIELONG 3 R/B, 65562 was space debris in LEO originally from a launch on Mon, 08 Sep 2025 UTC launched from the Yellow Sea Launch Area, China (YSLA). 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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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changzheng H.
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
500 kg wet, 500 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 1.1 m
Radar Cross Section
3.456 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 JIELONG 3 R/B
1 65562U 25201N 25261.01708302 .04598552 12062-4 33322-3 0 9990
2 65562 50.1317 215.7431 0117337 23.6976 336.9364 16.19249342 1456Epoch: 2025-09-18T00:24Z
TLE epoch observation values (Epoch: 2025-09-18T00:24:35.972Z)
Latitude
0.00001°
Longitude
-147.5915°
Altitude
151.078 km
Speed
7.859 km/s
True Right ascension
14h 22m 58s
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
07:21:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
299.82 km
Perigee altitude
144.923 km
Semi-major axis
6,600.509 km
Eccentricity
0.01173
Inclination
50.1317°
RAAN
215.7431°
Arg. of periapsis
23.6976°
True anomaly
336.40246°
Mean anomaly
336.9364°
Eccentric anomaly
336.67016°
Mean motion
4.04741 °/min
Orbital period
88.95 mins
BSTAR
0.00033322
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Other satellites on launch #201 in the year 2025 (2025-09-08 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 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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