GAOFEN 1-04, 43262
Orbit data source: Space-Track
GAOFEN 1-04, 43262 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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43262 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: 2 days ago
TLE from 2 days ago
0 GAOFEN 1-04
1 43262U 18031D 25286.42997343 .00000043 00000-0 13696-4 0 9990
2 43262 98.0898 344.2117 0001071 133.1324 226.9975 14.76441283406278Epoch: 2025-10-13T10:19Z
TLE epoch observation values (Epoch: 2025-10-13T10:19:09.704Z)
Latitude
-0.00003°
Longitude
167.1884°
Altitude
644.104 km
Speed
7.536 km/s
True Right ascension
22h 56m 50s
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
18:02:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
638.385 km
Perigee altitude
636.883 km
Semi-major axis
7,015.771 km
Eccentricity
0.00011
Inclination
98.0898°
RAAN
344.2117°
Arg. of periapsis
133.1324°
True anomaly
226.98853°
Mean anomaly
226.9975°
Eccentric anomaly
226.99301°
Mean motion
3.69343 °/min
Orbital period
97.47 mins
BSTAR
0.000013696
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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 1-04 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 | 2025-10-15 03:07:52.034Z | 116.296° SE | 2025-10-15 03:10:52.034Z | 63.196° ENE | 23.244° | 2025-10-15 03:13:52.034Z | 16.117° NNE |
| 5 mins | 2025-10-15 04:44:52.034Z | 220.493° SW | 2025-10-15 04:46:52.034Z | 259.709° W | 24.924° | 2025-10-15 04:49:52.034Z | 314.925° NW |
| 7 mins | 2025-10-15 16:34:52.034Z | 28.23° NE | 2025-10-15 16:37:52.034Z | 113.239° SE | 39.5° | 2025-10-15 16:41:52.034Z | 179.134° S |
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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