JILIN-01 GAOFEN 3D 6, 52391 (Decayed)
Orbit data source: Space-Track
JILIN-01 GAOFEN 3D 6, 52391 was a payload satellite owned by Changguang WJ (CN) in LEO that was launched on Sat, 30 Apr 2022 UTC via a CHANG ZHENG 11 launch vehicle from the Yellow Sea Launch Area, China (YSLA). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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52391 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Decayed Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
43 kg wet, 43 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.8 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 months ago
TLE from 2 months ago
0 JILIN-01 GAOFEN 3D 6
1 52391U 22046D 26121.28929000 .10941796 26287-5 40094-3 0 9993
2 52391 97.5003 244.2045 0012896 268.6399 91.3424 16.43001737223299Epoch: 2026-05-01T06:56Z
TLE epoch observation values (Epoch: 2026-05-01T06:56:34.655Z)
Latitude
-0.00003°
Longitude
-79.16358°
Altitude
161.29 km
Speed
7.809 km/s
True Right ascension
16h 16m 49s
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
21:35:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
163.063 km
Perigee altitude
146.213 km
Semi-major axis
6,532.775 km
Eccentricity
0.00129
Inclination
97.5003°
RAAN
244.2045°
Arg. of periapsis
268.6399°
True anomaly
91.49013°
Mean anomaly
91.3424°
Eccentric anomaly
91.41627°
Mean motion
4.11052 °/min
Orbital period
87.58 mins
BSTAR
0.00040094
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Other satellites on launch #46 in the year 2022 (2022-04-30 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.JILIN-01 GAOFEN 3D 6 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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