JIELONG 3 R/B, 65131 (Decayed)
Orbit data source: Space-Track
JIELONG 3 R/B, 65131 was space debris in LEO originally from a launch on Fri, 08 Aug 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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65131 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
2 weeks ago
Origin
CZHJ (CN / PRC)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
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & history
TLE from 2 weeks ago
0 JIELONG 3 R/B
1 65131U 25170N 25222.75348174 .20209411 14084-4 87823-4 0 9995
2 65131 50.1636 174.2758 0162424 353.8728 76.8326 16.29165810 324Epoch: 2025-08-10T18:05Z
TLE epoch observation values (Epoch: 2025-08-10T18:05:00.822Z)
Latitude
47.2495°
Longitude
7.35398°
Altitude
176.935 km
Speed
7.82 km/s
True Right ascension
15h 52m 18s
True Declination
47° 03' 46"
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
16:29:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
302.334 km
Perigee altitude
88.789 km
Semi-major axis
6,573.698 km
Eccentricity
0.01624
Inclination
50.1636°
RAAN
174.2758°
Arg. of periapsis
353.8728°
True anomaly
78.65302°
Mean anomaly
76.8326°
Eccentric anomaly
77.742°
Mean motion
4.07219 °/min
Orbital period
88.4 mins
BSTAR
0.000087823
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Other satellites on launch #170 in the year 2025 (2025-08-08 UTC)
JIELONG 3 R/B Visibility
Observer location: undefined°, undefined°
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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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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Authenticating...
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