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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Edit Public Description
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: 10 hours ago
TLE from 10 hours ago
0 GAOFEN 9 03
1 45794U 20039A 26002.31734229 .00015310 00000-0 54880-3 0 9992
2 45794 97.5158 133.8614 0012046 312.4362 47.5858 15.28754422308385Epoch: 2026-01-02T07:36Z
TLE epoch observation values (Epoch: 2026-01-02T07:36:58.373Z)
Latitude
-0.00005°
Longitude
-82.34111°
Altitude
477.066 km
Speed
7.63 km/s
True Right ascension
08h 55m 26s
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
17:40:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
484.751 km
Perigee altitude
468.237 km
Semi-major axis
6,854.631 km
Eccentricity
0.0012
Inclination
97.5158°
RAAN
133.8614°
Arg. of periapsis
312.4362°
True anomaly
47.68781°
Mean anomaly
47.5858°
Eccentric anomaly
47.6368°
Mean motion
3.82443 °/min
Orbital period
94.13 mins
BSTAR
0.0005488
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-01-02 20:45:32.392Z | 48.155° ENE | 2026-01-02 20:47:32.392Z | 85.441° E | 19.88° | 2026-01-02 20:50:32.392Z | 145.203° SSE |
| 4 mins | 2026-01-02 22:19:32.392Z | 325.325° NNW | 2026-01-02 22:21:32.392Z | 280.711° WNW | 19.348° | 2026-01-02 22:23:32.392Z | 244.226° WSW |
| 5 mins | 2026-01-03 08:53:32.392Z | 187.103° SSW | 2026-01-03 08:55:32.392Z | 269.908° W | 40.492° | 2026-01-03 08:58:32.392Z | 338.84° 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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