GAOFEN 1-02, 43259
Orbit data source: Space-Track
GAOFEN 1-02, 43259 is a payload satellite owned by GGKGJ (CN) in SSO that was launched on Sat, 31 Mar 2018 UTC via a CHANG ZHENG 4C launch vehicle from the Taiyaun Space Center, China (TSC). 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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43259 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
805 kg wet, ~700 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: 9 hours ago
TLE from 9 hours ago
0 GAOFEN 1-02
1 43259U 18031A 25291.62661399 .00000102 00000-0 22092-4 0 9999
2 43259 98.0878 349.3718 0003898 67.3653 292.7968 14.76404594407051Epoch: 2025-10-18T15:02Z
TLE epoch observation values (Epoch: 2025-10-18T15:02:19.448Z)
Latitude
-0.00008°
Longitude
96.43585°
Altitude
642.648 km
Speed
7.537 km/s
True Right ascension
23h 17m 29s
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
18:33:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.485 km
Perigee altitude
635.015 km
Semi-major axis
7,015.887 km
Eccentricity
0.00039
Inclination
98.0878°
RAAN
349.3718°
Arg. of periapsis
67.3653°
True anomaly
292.75561°
Mean anomaly
292.7968°
Eccentric anomaly
292.77621°
Mean motion
3.69334 °/min
Orbital period
97.47 mins
BSTAR
0.000022092
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Other satellites on launch #31 in the year 2018 (2018-03-31 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 1-02 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 | 2025-10-19 04:10:48.841Z | 179.778° S | 2025-10-19 04:13:48.841Z | 256.006° W | 42.27° | 2025-10-19 04:17:48.841Z | 340.313° N |
| 5 mins | 2025-10-19 16:02:48.841Z | 63.168° ENE | 2025-10-19 16:04:48.841Z | 103.301° ESE | 22.133° | 2025-10-19 16:07:48.841Z | 148.29° SSE |
| 5 mins | 2025-10-19 17:38:48.841Z | 333.968° NNW | 2025-10-19 17:40:48.841Z | 293.372° NW | 25.811° | 2025-10-19 17:43:48.841Z | 238.405° 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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