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 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: 14 hours ago
TLE from 14 hours ago
0 CFOSAT
1 43662U 18083A 25347.27409208 .00006276 00000-0 32623-3 0 9994
2 43662 97.3625 352.2733 0001922 136.9677 223.1706 15.16417203394268Epoch: 2025-12-13T06:34Z
TLE epoch observation values (Epoch: 2025-12-13T06:34:41.555Z)
Latitude
-0.00012°
Longitude
171.39645°
Altitude
520.733 km
Speed
7.602 km/s
True Right ascension
23h 29m 05s
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
18:46:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.973 km
Perigee altitude
512.324 km
Semi-major axis
6,891.785 km
Eccentricity
0.00019
Inclination
97.3625°
RAAN
352.2733°
Arg. of periapsis
136.9677°
True anomaly
223.15553°
Mean anomaly
223.1706°
Eccentric anomaly
223.16307°
Mean motion
3.79355 °/min
Orbital period
94.9 mins
BSTAR
0.00032623
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-14 00:07:53.522Z | 140.814° SSE | 2025-12-14 00:10:53.522Z | 71.601° E | 33.302° | 2025-12-14 00:13:53.522Z | 5.764° NNE |
| 5 mins | 2025-12-14 13:14:53.522Z | 21.873° NNE | 2025-12-14 13:16:53.522Z | 85.83° E | 42.99° | 2025-12-14 13:19:53.522Z | 183.392° SSW |
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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