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: 18 hours ago
TLE from 18 hours ago
0 CFOSAT
1 43662U 18083A 25256.34361564 .00002034 00000-0 10829-3 0 9995
2 43662 97.3654 264.0109 0001236 69.3559 290.7807 15.16318928380488Epoch: 2025-09-13T08:14Z
TLE epoch observation values (Epoch: 2025-09-13T08:14:48.391Z)
Latitude
0.00002°
Longitude
147.73094°
Altitude
519.761 km
Speed
7.604 km/s
True Right ascension
17h 36m 02s
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
19:03:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.798 km
Perigee altitude
513.094 km
Semi-major axis
6,892.083 km
Eccentricity
0.00012
Inclination
97.3654°
RAAN
264.0109°
Arg. of periapsis
69.3559°
True anomaly
290.76746°
Mean anomaly
290.7807°
Eccentric anomaly
290.77408°
Mean motion
3.7933 °/min
Orbital period
94.9 mins
BSTAR
0.00010829
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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 | 2025-09-14 13:18:40.298Z | 17.259° NNE | 2025-09-14 13:22:40.298Z | 147.573° SSE | 41.084° | 2025-09-14 13:25:40.298Z | 184.586° SSW |
| 5 mins | 2025-09-14 23:59:40.298Z | 116.556° SE | 2025-09-15 00:01:40.298Z | 70.052° E | 24.614° | 2025-09-15 00:04:40.298Z | 13.677° NNE |
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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