GAOFEN 3 03, 52200
Orbit data source: Space-Track
GAOFEN 3 03, 52200 is a payload satellite owned by GWHYZ (CN) in SSO that was launched on Wed, 06 Apr 2022 UTC via a CHANG ZHENG 4C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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52200 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
CAST
Mission
Operational Civil Radar Imaging
Bus & Motor
CS-L3000B, Unknown motor
Mass
~2,779 kg wet, ~2,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 3 Pan, 4.0 m
Radar Cross Section
10.846 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 GAOFEN 3 03
1 52200U 22035A 26172.53111140 .00000128 00000-0 51914-4 0 9990
2 52200 98.4063 181.0490 0001394 100.8391 259.2956 14.42215888221470Epoch: 2026-06-21T12:44Z
TLE epoch observation values (Epoch: 2026-06-21T12:44:48.024Z)
Latitude
-0.00001°
Longitude
80.11885°
Altitude
754.326 km
Speed
7.477 km/s
True Right ascension
12h 04m 11s
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
23:08:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
749.294 km
Perigee altitude
747.308 km
Semi-major axis
7,126.438 km
Eccentricity
0.00014
Inclination
98.4063°
RAAN
181.049°
Arg. of periapsis
100.8391°
True anomaly
259.2799°
Mean anomaly
259.2956°
Eccentric anomaly
259.28775°
Mean motion
3.60773 °/min
Orbital period
99.79 mins
BSTAR
0.000051914
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Other satellites on launch #35 in the year 2022 (2022-04-06 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.GAOFEN 3 03 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 12:39:00.924Z | 41.555° NE | 2026-06-22 12:43:00.924Z | 104.189° ESE | 24.965° | 2026-06-22 12:46:00.924Z | 148.347° SSE |
| 7 mins | 2026-06-22 14:18:00.924Z | 345.467° N | 2026-06-22 14:21:00.924Z | 298.143° NW | 27.535° | 2026-06-22 14:25:00.924Z | 234.218° WSW |
| 7 mins | 2026-06-22 23:52:00.924Z | 119.753° SE | 2026-06-22 23:55:00.924Z | 59.806° ENE | 29.41° | 2026-06-22 23:59:00.924Z | 5.684° NNE |
| 6 mins | 2026-06-23 01:31:00.924Z | 225.3° WSW | 2026-06-23 01:33:00.924Z | 257.572° W | 23.072° | 2026-06-23 01:37:00.924Z | 316.978° NNW |
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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