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: 9 hours ago
TLE from 9 hours ago
0 CFOSAT
1 43662U 18083A 26042.58628257 .00004654 00000-0 24249-3 0 9991
2 43662 97.3633 50.7996 0000275 69.5082 290.6181 15.16463434403409Epoch: 2026-02-11T14:04Z
TLE epoch observation values (Epoch: 2026-02-11T14:04:14.814Z)
Latitude
0.00002°
Longitude
58.0876°
Altitude
519.559 km
Speed
7.604 km/s
True Right ascension
03h 23m 11s
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
01:26:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.698 km
Perigee altitude
513.318 km
Semi-major axis
6,891.645 km
Eccentricity
0.00003
Inclination
97.3633°
RAAN
50.7996°
Arg. of periapsis
69.5082°
True anomaly
290.61515°
Mean anomaly
290.6181°
Eccentric anomaly
290.61663°
Mean motion
3.79366 °/min
Orbital period
94.9 mins
BSTAR
0.00024249
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-11 23:43:29.969Z | 113.153° SE | 2026-02-11 23:45:29.969Z | 73.109° E | 21.121° | 2026-02-11 23:48:29.969Z | 18.199° NNE |
| 4 mins | 2026-02-12 01:18:29.969Z | 239.509° WSW | 2026-02-12 01:19:29.969Z | 262.141° W | 20.296° | 2026-02-12 01:22:29.969Z | 316.424° NNW |
| 5 mins | 2026-02-12 12:49:29.969Z | 42.779° NE | 2026-02-12 12:51:29.969Z | 93.775° ESE | 29.773° | 2026-02-12 12:54:29.969Z | 160.963° 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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