GAOFEN 1-03, 43260
Orbit data source: Space-Track
GAOFEN 1-03, 43260 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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43260 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: 18 hours ago
TLE from 18 hours ago
0 GAOFEN 1-03
1 43260U 18031B 25341.28136176 .00001870 00000-0 27643-3 0 9998
2 43260 98.0803 38.9461 0002336 345.0519 15.0621 14.76420107414373Epoch: 2025-12-07T06:45Z
TLE epoch observation values (Epoch: 2025-12-07T06:45:09.656Z)
Latitude
0°
Longitude
-138.64113°
Altitude
642.075 km
Speed
7.538 km/s
True Right ascension
02h 35m 47s
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
23:02:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.34 km
Perigee altitude
636.062 km
Semi-major axis
7,015.838 km
Eccentricity
0.00023
Inclination
98.0803°
RAAN
38.9461°
Arg. of periapsis
345.0519°
True anomaly
15.06906°
Mean anomaly
15.0621°
Eccentric anomaly
15.06558°
Mean motion
3.69338 °/min
Orbital period
97.47 mins
BSTAR
0.00027643
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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 1-03 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-08 04:01:03.437Z | 166.81° S | 2025-12-08 04:05:03.437Z | 338.352° N | 44.361° | 2025-12-08 04:09:03.437Z | 346.881° N |
| 4 mins | 2025-12-08 15:54:03.437Z | 72.289° E | 2025-12-08 15:55:03.437Z | 89.212° E | 17.498° | 2025-12-08 15:58:03.437Z | 134.731° SE |
| 6 mins | 2025-12-08 17:29:03.437Z | 348.384° N | 2025-12-08 17:32:03.437Z | 284.139° WNW | 31.622° | 2025-12-08 17:35:03.437Z | 227.02° 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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