JIELONG 3 R/B, 67753 (Decayed)
Orbit data source: Space-Track
JIELONG 3 R/B, 67753 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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67753 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: 2 weeks ago
TLE from 2 weeks ago
0 JIELONG 3 R/B
1 67753U 26027H 26089.64278150 .14205116 23809-5 15616-3 0 9992
2 67753 97.4850 223.0801 0024595 183.4156 176.6984 16.48517197 7324Epoch: 2026-03-30T15:25Z
TLE epoch observation values (Epoch: 2026-03-30T15:25:36.321Z)
Latitude
-0.00003°
Longitude
163.64738°
Altitude
162.52 km
Speed
7.799 km/s
True Right ascension
14h 52m 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
21:44:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
156.075 km
Perigee altitude
124.012 km
Semi-major axis
6,518.181 km
Eccentricity
0.00246
Inclination
97.485°
RAAN
223.0801°
Arg. of periapsis
183.4156°
True anomaly
176.71458°
Mean anomaly
176.6984°
Eccentric anomaly
176.7065°
Mean motion
4.12433 °/min
Orbital period
87.29 mins
BSTAR
0.00015616
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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 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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