JILIN-01 GAOFEN 3D 31, 52448
Orbit data source: Space-Track
JILIN-01 GAOFEN 3D 31, 52448 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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52448 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 31
1 52448U 22048F 26163.81747469 .00159453 00000-0 84525-3 0 9997
2 52448 97.5689 278.6756 0001950 209.4400 150.6758 15.80094192228894Epoch: 2026-06-12T19:37Z
TLE epoch observation values (Epoch: 2026-06-12T19:37:09.813Z)
Latitude
0.00005°
Longitude
83.24323°
Altitude
334.481 km
Speed
7.707 km/s
True Right ascension
18h 34m 42s
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
12:47:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
328.375 km
Perigee altitude
325.76 km
Semi-major axis
6,705.204 km
Eccentricity
0.0002
Inclination
97.5689°
RAAN
278.6756°
Arg. of periapsis
209.44°
True anomaly
150.68674°
Mean anomaly
150.6758°
Eccentric anomaly
150.68127°
Mean motion
3.95298 °/min
Orbital period
91.07 mins
BSTAR
0.00084525
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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 31 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 | 2026-06-13 07:55:05.599Z | 186.876° SSW | 2026-06-13 07:57:05.599Z | 290.593° WNW | 36.505° | 2026-06-13 07:59:05.599Z | 336.594° NNW |
| 4 mins | 2026-06-13 20:30:05.599Z | 20.914° NNE | 2026-06-13 20:31:05.599Z | 40.075° NE | 39.097° | 2026-06-13 20:34:05.599Z | 186.927° SSW |
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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