GAOFEN 9 05, 46232
Orbit data source: Space-Track
GAOFEN 9 05, 46232 is a payload satellite owned by GGKGJ (CN) in SSO that was launched on Sun, 23 Aug 2020 UTC via a CHANG ZHENG 2D 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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46232 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Defense Imaging
Bus & Motor
CAST-3000, AOCS
Mass
~1,700 kg wet, ~1,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, Unknown HBR
Radar Cross Section
4.991 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 GAOFEN 9 05
1 46232U 20058A 26172.51673294 .00010639 00000-0 34553-3 0 9999
2 46232 97.2083 212.6889 0010119 83.8442 276.3953 15.32058121324276Epoch: 2026-06-21T12:24Z
TLE epoch observation values (Epoch: 2026-06-21T12:24:05.726Z)
Latitude
0.00003°
Longitude
116.94916°
Altitude
472.02 km
Speed
7.63 km/s
True Right ascension
14h 10m 45s
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
00:50:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
473.54 km
Perigee altitude
459.688 km
Semi-major axis
6,844.751 km
Eccentricity
0.00101
Inclination
97.2083°
RAAN
212.6889°
Arg. of periapsis
83.8442°
True anomaly
276.28005°
Mean anomaly
276.3953°
Eccentric anomaly
276.33768°
Mean motion
3.83272 °/min
Orbital period
93.93 mins
BSTAR
0.00034553
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Other satellites on launch #58 in the year 2020 (2020-08-23 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 9 05 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 15:36:42.635Z | 9.262° NNE | 2026-06-22 15:39:42.635Z | 213.492° SW | 43.028° | 2026-06-22 15:42:42.635Z | 195.447° SSW |
| 4 mins | 2026-06-23 02:10:42.635Z | 114.129° SE | 2026-06-23 02:12:42.635Z | 57.841° ENE | 24.222° | 2026-06-23 02:14:42.635Z | 17.415° NNE |
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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