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: 5 hours ago
TLE from 5 hours ago
0 GAOFEN 6
1 43484U 18048A 25297.85948743 .00001278 00000-0 19019-3 0 9998
2 43484 97.8090 3.7496 0010894 210.8996 149.1574 14.76541849398666Epoch: 2025-10-24T20:37Z
TLE epoch observation values (Epoch: 2025-10-24T20:37:39.713Z)
Latitude
-0.00009°
Longitude
20.8358°
Altitude
649.849 km
Speed
7.529 km/s
True Right ascension
00h 14m 59s
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
21:13:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
644.945 km
Perigee altitude
629.66 km
Semi-major axis
7,015.44 km
Eccentricity
0.00109
Inclination
97.809°
RAAN
3.7496°
Arg. of periapsis
210.8996°
True anomaly
149.22133°
Mean anomaly
149.1574°
Eccentric anomaly
149.18937°
Mean motion
3.69369 °/min
Orbital period
97.46 mins
BSTAR
0.00019019
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-25 03:18:13.062Z | 93.18° ESE | 2025-10-25 03:20:13.062Z | 64.529° ENE | 14.459° | 2025-10-25 03:22:13.062Z | 35.857° NE |
| 7 mins | 2025-10-25 04:53:13.062Z | 188.866° SSW | 2025-10-25 04:56:13.062Z | 255.958° W | 38.242° | 2025-10-25 05:00:13.062Z | 335.797° NNW |
| 6 mins | 2025-10-25 16:44:13.062Z | 43.795° NE | 2025-10-25 16:47:13.062Z | 105.177° ESE | 27.129° | 2025-10-25 16:50:13.062Z | 155.341° SSE |
| 5 mins | 2025-10-25 18:21:13.062Z | 328.746° NNW | 2025-10-25 18:23:13.062Z | 292.923° NW | 21.123° | 2025-10-25 18:26:13.062Z | 244.883° 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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