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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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: 7 hours ago
TLE from 7 hours ago
0 GAOFEN 1-03
1 43260U 18031B 26306.86750258 .00000373 00000-0 60987-4 0 9993
2 43260 98.0359 8.7208 0002476 9.4317 350.6939 14.76455473463159Epoch: 2026-11-02T20:49Z
TLE epoch observation values (Epoch: 2026-11-02T20:49:12.222Z)
Latitude
-0.00002°
Longitude
14.28152°
Altitude
641.832 km
Speed
7.538 km/s
True Right ascension
00h 34m 52s
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
23:47:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
639.324 km
Perigee altitude
635.849 km
Semi-major axis
7,015.724 km
Eccentricity
0.00025
Inclination
98.0359°
RAAN
8.7208°
Arg. of periapsis
9.4317°
True anomaly
350.68931°
Mean anomaly
350.6939°
Eccentric anomaly
350.69161°
Mean motion
3.69347 °/min
Orbital period
97.47 mins
BSTAR
0.000060987
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-03 05:04:45.024Z | 213.808° SW | 2026-11-03 05:07:45.024Z | 267.121° W | 26.5° | 2026-11-03 05:10:45.024Z | 316.927° NNW |
| 6 mins | 2026-11-03 16:55:45.024Z | 27.739° NE | 2026-11-03 16:58:45.024Z | 131.601° SE | 56.529° | 2026-11-03 17:01:45.024Z | 178.79° S |
| 6 mins | 2026-11-04 03:51:45.024Z | 138.838° SSE | 2026-11-04 03:54:45.024Z | 67.915° E | 46.902° | 2026-11-04 03:57:45.024Z | 4.986° NNE |
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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