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: 5 hours ago
TLE from 5 hours ago
0 GAOFEN 1-03
1 43260U 18031B 25295.19659251 .00001375 00000-0 20543-3 0 9992
2 43260 98.0872 352.8278 0004330 96.9292 263.2411 14.76382569407576Epoch: 2025-10-22T04:43Z
TLE epoch observation values (Epoch: 2025-10-22T04:43:05.592Z)
Latitude
0.00005°
Longitude
-108.81917°
Altitude
644.136 km
Speed
7.536 km/s
True Right ascension
23h 31m 18s
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
04:43:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
640.858 km
Perigee altitude
634.782 km
Semi-major axis
7,015.957 km
Eccentricity
0.00043
Inclination
98.0872°
RAAN
352.8278°
Arg. of periapsis
96.9292°
True anomaly
263.19183°
Mean anomaly
263.2411°
Eccentric anomaly
263.21646°
Mean motion
3.69328 °/min
Orbital period
97.47 mins
BSTAR
0.00020543
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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 | 2025-10-22 16:39:58.999Z | 18.593° NNE | 2025-10-22 16:43:58.999Z | 83.37° E | 42.485° | 2025-10-22 16:47:58.999Z | 183.748° SSW |
| 6 mins | 2025-10-23 03:37:58.999Z | 141.707° SSE | 2025-10-23 03:40:58.999Z | 53.374° ENE | 37.921° | 2025-10-23 03:43:58.999Z | 0.532° NNE |
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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