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: 15 hours ago
TLE from 15 hours ago
0 CFOSAT
1 43662U 18083A 26312.27532380 .00005031 00000-0 26278-3 0 9992
2 43662 97.3647 312.6061 0001520 71.4311 288.7088 15.16335730444279Epoch: 2026-11-08T06:36Z
TLE epoch observation values (Epoch: 2026-11-08T06:36:27.976Z)
Latitude
0.00006°
Longitude
166.02096°
Altitude
519.677 km
Speed
7.604 km/s
True Right ascension
20h 50m 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
17:35:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.943 km
Perigee altitude
512.848 km
Semi-major axis
6,892.032 km
Eccentricity
0.00015
Inclination
97.3647°
RAAN
312.6061°
Arg. of periapsis
71.4311°
True anomaly
288.6923°
Mean anomaly
288.7088°
Eccentric anomaly
288.70055°
Mean motion
3.79334 °/min
Orbital period
94.9 mins
BSTAR
0.00026278
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-09 00:09:05.437Z | 163.154° S | 2026-11-09 00:12:05.437Z | 133.27° SE | 72.813° | 2026-11-09 00:16:05.437Z | 350.515° N |
| 6 mins | 2026-11-09 13:16:05.437Z | 0.178° NNE | 2026-11-09 13:19:05.437Z | 250.626° W | 55.175° | 2026-11-09 13:22:05.437Z | 205.426° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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