JILIN-01 GAOFEN 3D 27, 52444
Orbit data source: Space-Track
JILIN-01 GAOFEN 3D 27, 52444 is a payload satellite owned by Changguang WJ (CN) in SSO that was launched on Thu, 05 May 2022 UTC via a CHANG ZHENG 2D launch vehicle from the Taiyaun Space Center, China (TSC). 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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52444 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Changguang WJ
Mission
Operational Commercial Imaging
Bus & Motor
JL-1, Unknown motor
Mass
42 kg wet, 42 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: 6 hours ago
TLE from 6 hours ago
0 JILIN-01 GAOFEN 3D 27
1 52444U 22048B 26163.83445529 .00115557 00000-0 79260-3 0 9994
2 52444 97.5704 277.3785 0001473 63.2043 296.9372 15.74370663228793Epoch: 2026-06-12T20:01Z
TLE epoch observation values (Epoch: 2026-06-12T20:01:36.937Z)
Latitude
0.00005°
Longitude
75.81638°
Altitude
349.133 km
Speed
7.7 km/s
True Right ascension
18h 29m 30s
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
12:46:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
344.314 km
Perigee altitude
342.334 km
Semi-major axis
6,721.461 km
Eccentricity
0.00015
Inclination
97.5704°
RAAN
277.3785°
Arg. of periapsis
63.2043°
True anomaly
296.92215°
Mean anomaly
296.9372°
Eccentric anomaly
296.92968°
Mean motion
3.93865 °/min
Orbital period
91.4 mins
BSTAR
0.0007926
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Other satellites on launch #48 in the year 2022 (2022-05-05 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 27 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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| JILIN-01 GAOFEN 3D 27 is likely not visible in the next few days. |
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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