GAOFEN 9 04, 46025
Orbit data source: Space-Track
GAOFEN 9 04, 46025 is a payload satellite owned by GGKGJ (CN) in SSO that was launched on Thu, 06 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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46025 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: 4 hours ago
TLE from 4 hours ago
0 GAOFEN 9 04
1 46025U 20054A 25261.30572352 .00008784 00000-0 30496-3 0 9993
2 46025 97.2802 329.8985 0011618 353.2342 6.8740 15.29942501284681Epoch: 2025-09-18T07:20Z
TLE epoch observation values (Epoch: 2025-09-18T07:20:14.512Z)
Latitude
-0.00001°
Longitude
-137.63119°
Altitude
471.184 km
Speed
7.635 km/s
True Right ascension
21h 59m 35s
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
04:18:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
480.891 km
Perigee altitude
464.972 km
Semi-major axis
6,851.068 km
Eccentricity
0.00116
Inclination
97.2802°
RAAN
329.8985°
Arg. of periapsis
353.2342°
True anomaly
6.88996°
Mean anomaly
6.874°
Eccentric anomaly
6.88198°
Mean motion
3.82742 °/min
Orbital period
94.06 mins
BSTAR
0.00030496
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Other satellites on launch #54 in the year 2020 (2020-08-06 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 9 04 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 | 2025-09-18 17:18:30.726Z | 19.85° NNE | 2025-09-18 17:21:30.726Z | 64.831° ENE | 38.709° | 2025-09-18 17:24:30.726Z | 177.027° S |
| 4 mins | 2025-09-19 05:27:30.726Z | 230.545° WSW | 2025-09-19 05:28:30.726Z | 253.215° W | 20.258° | 2025-09-19 05:31:30.726Z | 315.469° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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