QIANFAN-8, 60386
Orbit data source: Space-Track
QIANFAN-8, 60386 is a Chinese payload satellite in LEO that was launched on Tue, 06 Aug 2024 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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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60386 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-8
1 60386U 24140H 25326.34148478 .00000056 00000-0 67884-4 0 9999
2 60386 88.9745 301.3736 0014609 256.4837 103.4687 13.50974540 64595Epoch: 2025-11-22T08:11Z
TLE epoch observation values (Epoch: 2025-11-22T08:11:44.284Z)
Latitude
-0.00001°
Longitude
116.86754°
Altitude
1,074.178 km
Speed
7.314 km/s
True Right ascension
20h 05m 29s
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
14:21:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.601 km
Perigee altitude
1,054.852 km
Semi-major axis
7,443.863 km
Eccentricity
0.00146
Inclination
88.9745°
RAAN
301.3736°
Arg. of periapsis
256.4837°
True anomaly
103.63143°
Mean anomaly
103.4687°
Eccentric anomaly
103.55007°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000067884
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Other satellites on launch #140 in the year 2024 (2024-08-06 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.QIANFAN-8 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-22 22:30:25.755Z | 162.194° S | 2025-11-22 22:36:25.755Z | 102.297° ESE | 40.746° | 2025-11-22 22:42:25.755Z | 8.366° NNE |
| 8 mins | 2025-11-23 00:20:25.755Z | 244.972° WSW | 2025-11-23 00:23:25.755Z | 276.71° WNW | 19.844° | 2025-11-23 00:28:25.755Z | 327.502° NNW |
| 9 mins | 2025-11-23 09:42:25.755Z | 34.527° NE | 2025-11-23 09:46:25.755Z | 84.591° E | 25.964° | 2025-11-23 09:51:25.755Z | 137.553° SSE |
| 10 mins | 2025-11-23 11:28:25.755Z | 340.601° N | 2025-11-23 11:32:25.755Z | 289.342° WNW | 34.55° | 2025-11-23 11:38:25.755Z | 211.534° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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