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: 4 hours ago
TLE from 4 hours ago
0 CFOSAT
1 43662U 18083A 26084.88364765 .00003819 00000-0 19942-3 0 9997
2 43662 97.3640 91.8589 0002467 114.6900 245.4590 15.16491153409819Epoch: 2026-03-25T21:12Z
TLE epoch observation values (Epoch: 2026-03-25T21:12:27.156Z)
Latitude
-0.00009°
Longitude
-49.59479°
Altitude
520.249 km
Speed
7.603 km/s
True Right ascension
06h 07m 26s
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
06:51:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.124 km
Perigee altitude
511.724 km
Semi-major axis
6,891.561 km
Eccentricity
0.00025
Inclination
97.364°
RAAN
91.8589°
Arg. of periapsis
114.69°
True anomaly
245.43329°
Mean anomaly
245.459°
Eccentric anomaly
245.44614°
Mean motion
3.79373 °/min
Orbital period
94.89 mins
BSTAR
0.00019942
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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 | 2026-03-26 13:36:56.510Z | 351.993° N | 2026-03-26 13:38:56.510Z | 300.267° NW | 36.187° | 2026-03-26 13:41:56.510Z | 215.436° SW |
| 6 mins | 2026-03-27 00:15:56.510Z | 153.148° SSE | 2026-03-27 00:18:56.510Z | 35.392° NE | 39.861° | 2026-03-27 00:21:56.510Z | 355.271° N |
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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