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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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH
Mission
Operational Civil Science
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: 19 hours ago
TLE from 19 hours ago
0 CFOSAT
1 43662U 18083A 25260.30305090 .00004185 00000-0 21908-3 0 9997
2 43662 97.3653 267.8552 0001037 76.7026 283.4323 15.16350553381089Epoch: 2025-09-17T07:16Z
TLE epoch observation values (Epoch: 2025-09-17T07:16:23.597Z)
Latitude
-0.00003°
Longitude
162.27594°
Altitude
519.802 km
Speed
7.604 km/s
True Right ascension
17h 51m 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
18:46:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.565 km
Perigee altitude
513.136 km
Semi-major axis
6,891.987 km
Eccentricity
0.0001
Inclination
97.3653°
RAAN
267.8552°
Arg. of periapsis
76.7026°
True anomaly
283.42074°
Mean anomaly
283.4323°
Eccentric anomaly
283.42652°
Mean motion
3.79338 °/min
Orbital period
94.9 mins
BSTAR
0.00021908
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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 | 2025-09-18 13:56:22.479Z | 342.294° N | 2025-09-18 13:58:22.479Z | 285.756° WNW | 31.648° | 2025-09-18 14:01:22.479Z | 221.13° SW |
| 6 mins | 2025-09-19 00:35:22.479Z | 162.535° S | 2025-09-19 00:37:22.479Z | 138.726° SSE | 43.621° | 2025-09-19 00:41:22.479Z | 350.22° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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