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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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: 4 hours ago
TLE from 4 hours ago
0 GAOFEN 6
1 43484U 18048A 26085.33049299 .00000502 00000-0 78787-4 0 9992
2 43484 97.7834 151.0211 0013675 86.0658 274.2116 14.76623543421167Epoch: 2026-03-26T07:55Z
TLE epoch observation values (Epoch: 2026-03-26T07:55:54.594Z)
Latitude
0.00003°
Longitude
-151.73737°
Altitude
642.331 km
Speed
7.537 km/s
True Right ascension
10h 04m 05s
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
17:15:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
646.636 km
Perigee altitude
627.449 km
Semi-major axis
7,015.179 km
Eccentricity
0.00137
Inclination
97.7834°
RAAN
151.0211°
Arg. of periapsis
86.0658°
True anomaly
274.0553°
Mean anomaly
274.2116°
Eccentric anomaly
274.13345°
Mean motion
3.6939 °/min
Orbital period
97.46 mins
BSTAR
0.000078787
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-26 16:38:49.341Z | 36.484° NE | 2026-03-26 16:41:49.341Z | 96.405° ESE | 31.046° | 2026-03-26 16:45:49.341Z | 165.264° S |
| 4 mins | 2026-03-26 18:16:49.341Z | 316.113° NNW | 2026-03-26 18:17:49.341Z | 298.727° NW | 18.199° | 2026-03-26 18:20:49.341Z | 251.838° W |
| 6 mins | 2026-03-27 03:35:49.341Z | 119.156° SE | 2026-03-27 03:38:49.341Z | 59.419° ENE | 25.394° | 2026-03-27 03:41:49.341Z | 12.843° NNE |
| 5 mins | 2026-03-27 05:12:49.341Z | 226.321° WSW | 2026-03-27 05:14:49.341Z | 263.143° W | 21.958° | 2026-03-27 05:17:49.341Z | 313.585° NW |
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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