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: 6 hours ago
TLE from 6 hours ago
0 GAOFEN 1-03
1 43260U 18031B 25311.86873743 .00001558 00000-0 23154-3 0 9993
2 43260 98.0847 9.5155 0004034 59.4237 300.7370 14.76431150410039Epoch: 2025-11-07T20:50Z
TLE epoch observation values (Epoch: 2025-11-07T20:50:58.913Z)
Latitude
-0.00005°
Longitude
9.46351°
Altitude
642.176 km
Speed
7.538 km/s
True Right ascension
00h 38m 03s
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
23:07:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.496 km
Perigee altitude
634.836 km
Semi-major axis
7,015.803 km
Eccentricity
0.0004
Inclination
98.0847°
RAAN
9.5155°
Arg. of periapsis
59.4237°
True anomaly
300.69726°
Mean anomaly
300.737°
Eccentric anomaly
300.71713°
Mean motion
3.69341 °/min
Orbital period
97.47 mins
BSTAR
0.00023154
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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
Loading observer location...
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 | 2025-11-08 03:29:22.035Z | 137.746° SSE | 2025-11-08 03:32:22.035Z | 83.644° E | 33.454° | 2025-11-08 03:36:22.035Z | 3.751° NNE |
| 6 mins | 2025-11-08 16:57:22.035Z | 9.782° NNE | 2025-11-08 16:59:22.035Z | 354.32° N | 43.351° | 2025-11-08 17:03:22.035Z | 197.081° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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