GAOFEN 9 03, 45794
Orbit data source: Space-Track
GAOFEN 9 03, 45794 is a payload satellite owned by GGKGJ (CN) in SSO that was launched on Wed, 17 Jun 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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45794 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: 12 hours ago
TLE from 12 hours ago
0 GAOFEN 9 03
1 45794U 20039A 26092.31480167 .00014885 00000-0 49689-3 0 9997
2 45794 97.5264 224.9445 0011404 358.4985 1.6220 15.31086749322143Epoch: 2026-04-02T07:33Z
TLE epoch observation values (Epoch: 2026-04-02T07:33:18.864Z)
Latitude
0.00003°
Longitude
-79.04916°
Altitude
467.859 km
Speed
7.637 km/s
True Right ascension
14h 59m 46s
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
01:06:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
477.334 km
Perigee altitude
461.716 km
Semi-major axis
6,847.662 km
Eccentricity
0.00114
Inclination
97.5264°
RAAN
224.9445°
Arg. of periapsis
358.4985°
True anomaly
1.6257°
Mean anomaly
1.622°
Eccentric anomaly
1.62385°
Mean motion
3.83027 °/min
Orbital period
93.99 mins
BSTAR
0.00049689
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Other satellites on launch #39 in the year 2020 (2020-06-17 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 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-04-02 22:14:36.019Z | 334.9° NNW | 2026-04-02 22:16:36.019Z | 278.489° WNW | 26.61° | 2026-04-02 22:18:36.019Z | 233.476° WSW |
| 5 mins | 2026-04-03 08:47:36.019Z | 162.755° S | 2026-04-03 08:49:36.019Z | 76.79° E | 44.742° | 2026-04-03 08:52:36.019Z | 350.015° N |
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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