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: 12 hours ago
TLE from 12 hours ago
0 GAOFEN 6
1 43484U 18048A 25260.31784562 .00000671 00000-0 10309-3 0 9995
2 43484 97.8146 327.4275 0011616 342.2597 17.8206 14.76604923393121Epoch: 2025-09-17T07:37Z
TLE epoch observation values (Epoch: 2025-09-17T07:37:41.861Z)
Latitude
-0.00005°
Longitude
-143.49244°
Altitude
635.319 km
Speed
7.545 km/s
True Right ascension
21h 49m 42s
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
12:47:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
645.252 km
Perigee altitude
628.954 km
Semi-major axis
7,015.24 km
Eccentricity
0.00116
Inclination
97.8146°
RAAN
327.4275°
Arg. of periapsis
342.2597°
True anomaly
17.86139°
Mean anomaly
17.8206°
Eccentric anomaly
17.84099°
Mean motion
3.69385 °/min
Orbital period
97.46 mins
BSTAR
0.00010309
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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 | 2025-09-18 04:54:17.858Z | 189.613° SSW | 2025-09-18 04:57:17.858Z | 280.644° WNW | 38.483° | 2025-09-18 05:00:17.858Z | 334.6° NNW |
| 6 mins | 2025-09-18 16:45:17.858Z | 50.845° ENE | 2025-09-18 16:47:17.858Z | 91.098° ESE | 26.484° | 2025-09-18 16:51:17.858Z | 157.315° SSE |
| 5 mins | 2025-09-18 18:22:17.858Z | 322.415° NNW | 2025-09-18 18:24:17.858Z | 282.576° WNW | 21.969° | 2025-09-18 18:27:17.858Z | 239.415° WSW |
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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