CFOSAT, 43662
Orbit data source: Space-Track
CFOSAT, 43662 is a Chinese payload satellite in SSO that was launched on Mon, 29 Oct 2018 UTC via a CHANG ZHENG 2C launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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43662 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Civil Earth Obs Sci
Bus & Motor
CAST-2000, Unknown motor
Mass
700 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 5.0 m
Radar Cross Section
5.252 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 CFOSAT
1 43662U 18083A 26193.82813308 .00001813 00000-0 96316-4 0 9997
2 43662 97.3615 197.6056 0001912 75.6097 284.5349 15.16526739426322Epoch: 2026-07-12T19:52Z
TLE epoch observation values (Epoch: 2026-07-12T19:52:30.698Z)
Latitude
0.00005°
Longitude
-31.24372°
Altitude
519.104 km
Speed
7.604 km/s
True Right ascension
13h 10m 25s
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
16:02:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.634 km
Perigee altitude
511.998 km
Semi-major axis
6,891.453 km
Eccentricity
0.00019
Inclination
97.3615°
RAAN
197.6056°
Arg. of periapsis
75.6097°
True anomaly
284.51369°
Mean anomaly
284.5349°
Eccentric anomaly
284.5243°
Mean motion
3.79382 °/min
Orbital period
94.89 mins
BSTAR
0.000096316
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Other satellites on launch #83 in the year 2018 (2018-10-29 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.CFOSAT 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-07-13 12:18:01.446Z | 58.832° ENE | 2026-07-13 12:20:01.446Z | 97.574° ESE | 17.774° | 2026-07-13 12:22:01.446Z | 133.887° SE |
| 5 mins | 2026-07-13 13:52:01.446Z | 332.566° NNW | 2026-07-13 13:54:01.446Z | 286.318° WNW | 23.789° | 2026-07-13 13:57:01.446Z | 232.01° WSW |
| 5 mins | 2026-07-14 00:31:01.446Z | 181.295° SSW | 2026-07-14 00:33:01.446Z | 232.945° WSW | 41.79° | 2026-07-14 00:36:01.446Z | 339.426° N |
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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