JIELONG 3 DEB, 67754 (Decayed)
Orbit data source: Space-Track
JIELONG 3 DEB, 67754 was space debris in LEO originally from a Chinese launch on Thu, 12 Feb 2026 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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67754 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 month ago
TLE from 1 month ago
0 JIELONG 3 DEB
1 67754U 26027J 26068.58541937 .12424544 23987-5 30812-3 0 9997
2 67754 97.4912 200.1849 0053557 253.0553 106.4871 16.38523310 3940Epoch: 2026-03-09T14:03Z
TLE epoch observation values (Epoch: 2026-03-09T14:03:00.233Z)
Latitude
0°
Longitude
-177.84232°
Altitude
183.107 km
Speed
7.79 km/s
True Right ascension
13h 20m 44s
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
20:04:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
201.599 km
Perigee altitude
131.496 km
Semi-major axis
6,544.684 km
Eccentricity
0.00536
Inclination
97.4912°
RAAN
200.1849°
Arg. of periapsis
253.0553°
True anomaly
107.07446°
Mean anomaly
106.4871°
Eccentric anomaly
106.78089°
Mean motion
4.0993 °/min
Orbital period
87.82 mins
BSTAR
0.00030812
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Other satellites on launch #27 in the year 2026 (2026-02-12 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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