JILIN-01 GAOFEN 3D 29, 52446
Orbit data source: Space-Track
JILIN-01 GAOFEN 3D 29, 52446 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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52446 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: 7 hours ago
TLE from 7 hours ago
0 JILIN-01 GAOFEN 3D 29
1 52446U 22048D 26168.07968764 .00110367 00000-0 72211-3 0 9991
2 52446 97.5715 282.3627 0001097 249.5842 110.5305 15.75481195229484Epoch: 2026-06-17T01:54Z
TLE epoch observation values (Epoch: 2026-06-17T01:54:45.012Z)
Latitude
0.00002°
Longitude
-11.66737°
Altitude
346.681 km
Speed
7.701 km/s
True Right ascension
18h 49m 27s
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
19:31:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
340.899 km
Perigee altitude
339.425 km
Semi-major axis
6,718.299 km
Eccentricity
0.00011
Inclination
97.5715°
RAAN
282.3627°
Arg. of periapsis
249.5842°
True anomaly
110.54227°
Mean anomaly
110.5305°
Eccentric anomaly
110.53639°
Mean motion
3.94143 °/min
Orbital period
91.34 mins
BSTAR
0.00072211
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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 29 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-17 20:45:29.146Z | 357.539° N | 2026-06-17 20:47:29.146Z | 289.099° WNW | 37.11° | 2026-06-17 20:49:29.146Z | 212.619° SW |
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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