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: 8 hours ago
TLE from 8 hours ago
0 GAOFEN 1-03
1 43260U 18031B 25259.61717101 .00000596 00000-0 93268-4 0 9997
2 43260 98.0021 317.2042 0003770 189.0604 171.0539 14.76308482402321Epoch: 2025-09-16T14:48Z
TLE epoch observation values (Epoch: 2025-09-16T14:48:43.575Z)
Latitude
0.00007°
Longitude
99.21773°
Altitude
646.629 km
Speed
7.533 km/s
True Right ascension
21h 08m 49s
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
15:58:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.696 km
Perigee altitude
635.406 km
Semi-major axis
7,016.188 km
Eccentricity
0.00038
Inclination
98.0021°
RAAN
317.2042°
Arg. of periapsis
189.0604°
True anomaly
171.06061°
Mean anomaly
171.0539°
Eccentric anomaly
171.05726°
Mean motion
3.6931 °/min
Orbital period
97.48 mins
BSTAR
0.000093268
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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 | 2025-09-17 03:56:50.025Z | 167.365° S | 2025-09-17 04:00:50.025Z | 337.553° N | 43.851° | 2025-09-17 04:04:50.025Z | 346.799° N |
| 4 mins | 2025-09-17 15:49:50.025Z | 72.811° E | 2025-09-17 15:50:50.025Z | 90.104° ESE | 17.838° | 2025-09-17 15:53:50.025Z | 135.819° SSE |
| 6 mins | 2025-09-17 17:24:50.025Z | 347.283° N | 2025-09-17 17:27:50.025Z | 282.808° WNW | 30.937° | 2025-09-17 17:30:50.025Z | 227.447° 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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