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: 5 hours ago
TLE from 5 hours ago
0 GAOFEN 6
1 43484U 18048A 26265.32437927 -.00000091 00000-0 -54677-5 0 9998
2 43484 98.0876 328.1551 0009791 212.7683 147.2920 14.76443786447722Epoch: 2026-09-22T07:47Z
TLE epoch observation values (Epoch: 2026-09-22T07:47:06.368Z)
Latitude
-0.00007°
Longitude
-149.81291°
Altitude
649.368 km
Speed
7.53 km/s
True Right ascension
21h 52m 37s
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
05:51:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
644.495 km
Perigee altitude
630.757 km
Semi-major axis
7,015.763 km
Eccentricity
0.00098
Inclination
98.0876°
RAAN
328.1551°
Arg. of periapsis
212.7683°
True anomaly
147.35256°
Mean anomaly
147.292°
Eccentric anomaly
147.32229°
Mean motion
3.69344 °/min
Orbital period
97.47 mins
BSTAR
-0.0000054677
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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 | 2026-09-22 16:29:51.447Z | 37.737° NE | 2026-09-22 16:32:51.447Z | 84.479° E | 29.652° | 2026-09-22 16:36:51.447Z | 156.347° SSE |
| 5 mins | 2026-09-22 18:07:51.447Z | 326.339° NNW | 2026-09-22 18:09:51.447Z | 288.216° WNW | 23.613° | 2026-09-22 18:12:51.447Z | 242.179° WSW |
| 5 mins | 2026-09-23 03:27:51.447Z | 107.207° ESE | 2026-09-23 03:29:51.447Z | 69.581° E | 25.553° | 2026-09-23 03:32:51.447Z | 19.085° NNE |
| 6 mins | 2026-09-23 05:03:51.447Z | 216.535° SW | 2026-09-23 05:05:51.447Z | 252.87° W | 28.103° | 2026-09-23 05:09:51.447Z | 321.656° 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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