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 25359.86457495 .00000585 00000-0 90786-4 0 9998
2 43484 97.8010 63.6895 0012500 24.5322 335.6481 14.76587742407814Epoch: 2025-12-25T20:44Z
TLE epoch observation values (Epoch: 2025-12-25T20:44:59.275Z)
Latitude
0°
Longitude
17.82903°
Altitude
635.143 km
Speed
7.545 km/s
True Right ascension
04h 14m 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
01:59:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
645.926 km
Perigee altitude
628.388 km
Semi-major axis
7,015.294 km
Eccentricity
0.00125
Inclination
97.801°
RAAN
63.6895°
Arg. of periapsis
24.5322°
True anomaly
335.58895°
Mean anomaly
335.6481°
Eccentric anomaly
335.61853°
Mean motion
3.69381 °/min
Orbital period
97.46 mins
BSTAR
0.000090786
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-26 03:24:49.603Z | 104.234° ESE | 2025-12-26 03:26:49.603Z | 73.781° E | 17.78° | 2025-12-26 03:29:49.603Z | 26.489° NE |
| 6 mins | 2025-12-26 05:00:49.603Z | 203.992° SW | 2025-12-26 05:03:49.603Z | 274.322° WNW | 30.992° | 2025-12-26 05:06:49.603Z | 326.436° NNW |
| 6 mins | 2025-12-26 16:51:49.603Z | 42.1° NE | 2025-12-26 16:53:49.603Z | 91.229° ESE | 33.801° | 2025-12-26 16:57:49.603Z | 168.229° S |
| 4 mins | 2025-12-26 18:28:49.603Z | 316.727° NNW | 2025-12-26 18:29:49.603Z | 300.583° NW | 16.737° | 2025-12-26 18:32:49.603Z | 255.567° W |
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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