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: 9 hours ago
TLE from 9 hours ago
0 GAOFEN 1-04
1 43262U 18031D 25312.52197487 .00001570 00000-0 23301-3 0 9991
2 43262 98.0855 10.3348 0002007 100.5439 259.5996 14.76457837410129Epoch: 2025-11-08T12:31Z
TLE epoch observation values (Epoch: 2025-11-08T12:31:38.628Z)
Latitude
-0.0001°
Longitude
134.47348°
Altitude
643.793 km
Speed
7.536 km/s
True Right ascension
00h 41m 20s
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
17:41:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
638.989 km
Perigee altitude
636.173 km
Semi-major axis
7,015.718 km
Eccentricity
0.0002
Inclination
98.0855°
RAAN
10.3348°
Arg. of periapsis
100.5439°
True anomaly
259.57698°
Mean anomaly
259.5996°
Eccentric anomaly
259.58829°
Mean motion
3.69347 °/min
Orbital period
97.47 mins
BSTAR
0.00023301
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-09 03:17:40.356Z | 131.573° SE | 2025-11-09 03:21:40.356Z | 64.726° ENE | 27.549° | 2025-11-09 03:24:40.356Z | 12.745° NNE |
| 5 mins | 2025-11-09 04:55:40.356Z | 225.168° WSW | 2025-11-09 04:57:40.356Z | 258.553° W | 20.528° | 2025-11-09 05:00:40.356Z | 309.309° NW |
| 7 mins | 2025-11-09 16:45:40.356Z | 20.207° NNE | 2025-11-09 16:48:40.356Z | 115.441° SE | 43.545° | 2025-11-09 16:52:40.356Z | 186.63° SSW |
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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