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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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 1-04
1 43262U 18031D 26307.85985326 -.00000396 00000-0 -49548-4 0 9998
2 43262 98.0369 9.9164 0001084 43.4571 316.6724 14.76454237463296Epoch: 2026-11-03T20:38Z
TLE epoch observation values (Epoch: 2026-11-03T20:38:11.321Z)
Latitude
-0.00002°
Longitude
17.25277°
Altitude
642.998 km
Speed
7.537 km/s
True Right ascension
00h 39m 39s
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
22:08:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
638.351 km
Perigee altitude
636.83 km
Semi-major axis
7,015.728 km
Eccentricity
0.00011
Inclination
98.0369°
RAAN
9.9164°
Arg. of periapsis
43.4571°
True anomaly
316.66388°
Mean anomaly
316.6724°
Eccentric anomaly
316.66814°
Mean motion
3.69347 °/min
Orbital period
97.47 mins
BSTAR
-0.000049548
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-04 03:17:56.016Z | 106.785° ESE | 2026-11-04 03:19:56.016Z | 76.11° E | 20.319° | 2026-11-04 03:22:56.016Z | 26.501° NE |
| 6 mins | 2026-11-04 04:53:56.016Z | 205.371° SW | 2026-11-04 04:56:56.016Z | 269.988° W | 35.098° | 2026-11-04 04:59:56.016Z | 323.603° NNW |
| 6 mins | 2026-11-04 16:44:56.016Z | 38.232° NE | 2026-11-04 16:46:56.016Z | 81.39° E | 42.663° | 2026-11-04 16:50:56.016Z | 168.524° S |
| 4 mins | 2026-11-04 18:21:56.016Z | 319.96° NNW | 2026-11-04 18:23:56.016Z | 287.777° WNW | 16.933° | 2026-11-04 18:25:56.016Z | 259.095° W |
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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