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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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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-8
1 60386U 24140H 26118.80065264 .00000054 00000-0 65197-4 0 9994
2 60386 88.9692 285.0538 0017485 156.4941 203.7013 13.51007989 85858Epoch: 2026-04-28T19:12Z
TLE epoch observation values (Epoch: 2026-04-28T19:12:56.388Z)
Latitude
-0°
Longitude
140.04809°
Altitude
1,083.434 km
Speed
7.305 km/s
True Right ascension
19h 00m 12s
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
10:08:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.619 km
Perigee altitude
1,052.588 km
Semi-major axis
7,443.74 km
Eccentricity
0.00175
Inclination
88.9692°
RAAN
285.0538°
Arg. of periapsis
156.4941°
True anomaly
203.62092°
Mean anomaly
203.7013°
Eccentric anomaly
203.66109°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.000065197
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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 | 2026-04-29 11:19:13.211Z | 170.323° S | 2026-04-29 11:24:13.211Z | 124.687° SE | 43.91° | 2026-04-29 11:31:13.211Z | 2.224° NNE |
| 6 mins | 2026-04-29 13:09:13.211Z | 257.866° W | 2026-04-29 13:12:13.211Z | 287.959° WNW | 15.536° | 2026-04-29 13:15:13.211Z | 316.603° NNW |
| 10 mins | 2026-04-29 22:29:13.211Z | 23.109° NE | 2026-04-29 22:34:13.211Z | 87.299° E | 30.962° | 2026-04-29 22:39:13.211Z | 146.01° SSE |
| 9 mins | 2026-04-30 00:16:13.211Z | 334.521° NNW | 2026-04-30 00:20:13.211Z | 285.098° WNW | 29.196° | 2026-04-30 00:25:13.211Z | 223.893° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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