GAOFEN 6, 43484
Orbit data source: Space-Track
GAOFEN 6, 43484 is a payload satellite owned by GGKGJ (CN) in SSO that was launched on Sat, 02 Jun 2018 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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43484 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Civil Imaging
Bus & Motor
CAST-2000, AOCS
Mass
1,064 kg wet, ~900 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
4.991 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 GAOFEN 6
1 43484U 18048A 25351.32616520 .00000376 00000-0 60965-4 0 9991
2 43484 97.8032 55.4392 0013009 50.0191 310.2160 14.76574014406553Epoch: 2025-12-17T07:49Z
TLE epoch observation values (Epoch: 2025-12-17T07:49:40.673Z)
Latitude
0.00004°
Longitude
-148.17791°
Altitude
637.29 km
Speed
7.543 km/s
True Right ascension
03h 41m 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
12:56:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
646.327 km
Perigee altitude
628.074 km
Semi-major axis
7,015.337 km
Eccentricity
0.0013
Inclination
97.8032°
RAAN
55.4392°
Arg. of periapsis
50.0191°
True anomaly
310.10205°
Mean anomaly
310.216°
Eccentric anomaly
310.15904°
Mean motion
3.69377 °/min
Orbital period
97.46 mins
BSTAR
0.000060965
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Other satellites on launch #48 in the year 2018 (2018-06-02 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 6 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 | 2025-12-17 16:32:41.012Z | 43.481° NE | 2025-12-17 16:35:41.012Z | 94.194° ESE | 23.923° | 2025-12-17 16:38:41.012Z | 146.47° SSE |
| 6 mins | 2025-12-17 18:09:41.012Z | 337.02° NNW | 2025-12-17 18:12:41.012Z | 279.188° WNW | 23.738° | 2025-12-17 18:15:41.012Z | 235.409° WSW |
| 5 mins | 2025-12-18 03:30:41.012Z | 99.258° ESE | 2025-12-18 03:32:41.012Z | 63.311° ENE | 19.647° | 2025-12-18 03:35:41.012Z | 19.269° NNE |
| 6 mins | 2025-12-18 05:06:41.012Z | 214.796° SW | 2025-12-18 05:08:41.012Z | 259.752° W | 28.794° | 2025-12-18 05:12:41.012Z | 327.696° 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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