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: 3 days ago
TLE from 3 days ago
0 GAOFEN 1-03
1 43260U 18031B 25254.05979154 .00000695 00000-0 10662-3 0 9994
2 43260 97.8001 311.7496 0005240 199.0406 161.0610 14.76587976401508Epoch: 2025-09-11T01:26Z
TLE epoch observation values (Epoch: 2025-09-11T01:26:05.989Z)
Latitude
0.00008°
Longitude
-60.10265°
Altitude
646.614 km
Speed
7.533 km/s
True Right ascension
20h 46m 59s
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
01:51:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.832 km
Perigee altitude
633.48 km
Semi-major axis
7,015.293 km
Eccentricity
0.00052
Inclination
97.8001°
RAAN
311.7496°
Arg. of periapsis
199.0406°
True anomaly
161.08048°
Mean anomaly
161.061°
Eccentric anomaly
161.07074°
Mean motion
3.69381 °/min
Orbital period
97.46 mins
BSTAR
0.00010662
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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 | 2025-09-14 16:12:24.857Z | 33.084° NE | 2025-09-14 16:16:24.857Z | 107.751° ESE | 29.551° | 2025-09-14 16:19:24.857Z | 159.348° S |
| 5 mins | 2025-09-14 17:50:24.857Z | 326.225° NNW | 2025-09-14 17:52:24.857Z | 291.909° WNW | 19.27° | 2025-09-14 17:55:24.857Z | 247.015° WSW |
| 5 mins | 2025-09-15 03:10:24.857Z | 112.539° SE | 2025-09-15 03:12:24.857Z | 74.105° E | 24.916° | 2025-09-15 03:15:24.857Z | 19.098° NNE |
| 6 mins | 2025-09-15 04:46:24.857Z | 217.723° SW | 2025-09-15 04:49:24.857Z | 272.481° WNW | 23.077° | 2025-09-15 04:52:24.857Z | 318.456° 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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