JIELONG 3 DEB, 65561 (Decayed)
Orbit data source: Space-Track
JIELONG 3 DEB, 65561 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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65561 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: 3 months ago
TLE from 3 months ago
0 JIELONG 3 DEB
1 65561U 25201M 26081.83395989 .16342055 12297-4 57747-3 0 9998
2 65561 50.0458 335.5800 0005293 183.1623 176.9350 16.44201711 30375Epoch: 2026-03-22T20:00Z
TLE epoch observation values (Epoch: 2026-03-22T20:00:54.134Z)
Latitude
-0.00002°
Longitude
-144.98021°
Altitude
158.69 km
Speed
7.81 km/s
True Right ascension
22h 22m 19s
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
07:22:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
158.911 km
Perigee altitude
151.994 km
Semi-major axis
6,533.59 km
Eccentricity
0.00053
Inclination
50.0458°
RAAN
335.58°
Arg. of periapsis
183.1623°
True anomaly
176.93824°
Mean anomaly
176.935°
Eccentric anomaly
176.93662°
Mean motion
4.10975 °/min
Orbital period
87.6 mins
BSTAR
0.00057747
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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 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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