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: 1 day ago
TLE from 1 day ago
0 GAOFEN 1-03
1 43260U 18031B 25259.68494861 .00000560 00000-0 88093-4 0 9990
2 43260 98.0021 317.2713 0003777 188.8316 171.2828 14.76308378402338Epoch: 2025-09-16T16:26Z
TLE epoch observation values (Epoch: 2025-09-16T16:26:19.559Z)
Latitude
-0.00003°
Longitude
74.8181°
Altitude
646.636 km
Speed
7.533 km/s
True Right ascension
21h 09m 05s
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
08:49:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.701 km
Perigee altitude
635.401 km
Semi-major axis
7,016.188 km
Eccentricity
0.00038
Inclination
98.0021°
RAAN
317.2713°
Arg. of periapsis
188.8316°
True anomaly
171.28936°
Mean anomaly
171.2828°
Eccentric anomaly
171.28608°
Mean motion
3.6931 °/min
Orbital period
97.48 mins
BSTAR
0.000088093
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-17 17:23:42.394Z | 355.102° N | 2025-09-17 17:27:42.394Z | 287.009° WNW | 31.033° | 2025-09-17 17:30:42.394Z | 228.439° WSW |
| 4 mins | 2025-09-18 02:46:42.394Z | 86.163° E | 2025-09-18 02:47:42.394Z | 70.683° E | 15.481° | 2025-09-18 02:50:42.394Z | 27.524° NE |
| 6 mins | 2025-09-18 04:21:42.394Z | 197.3° SSW | 2025-09-18 04:23:42.394Z | 239.982° WSW | 35.162° | 2025-09-18 04:27:42.394Z | 331.546° 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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