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: 5 hours ago
TLE from 5 hours ago
0 QIANFAN-8
1 60386U 24140H 26054.51396501 .00000093 00000-0 12516-3 0 9991
2 60386 88.9739 291.7430 0016641 354.0839 6.0113 13.51001430 77176Epoch: 2026-02-23T12:20Z
TLE epoch observation values (Epoch: 2026-02-23T12:20:06.576Z)
Latitude
-0.00004°
Longitude
-46.69116°
Altitude
1,059.203 km
Speed
7.328 km/s
True Right ascension
19h 26m 58s
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
20:21:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.015 km
Perigee altitude
1,053.24 km
Semi-major axis
7,443.764 km
Eccentricity
0.00166
Inclination
88.9739°
RAAN
291.743°
Arg. of periapsis
354.0839°
True anomaly
6.03131°
Mean anomaly
6.0113°
Eccentric anomaly
6.0213°
Mean motion
3.37951 °/min
Orbital period
106.52 mins
BSTAR
0.00012516
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-23 17:48:56.063Z | 250.186° W | 2026-02-23 17:51:56.063Z | 278.947° WNW | 15.805° | 2026-02-23 17:55:56.063Z | 318.366° NNW |
| 10 mins | 2026-02-24 03:09:56.063Z | 24.585° NE | 2026-02-24 03:14:56.063Z | 89.13° E | 30.524° | 2026-02-24 03:19:56.063Z | 145.291° SSE |
| 10 mins | 2026-02-24 04:56:56.063Z | 334.387° NNW | 2026-02-24 05:00:56.063Z | 283.243° WNW | 30.281° | 2026-02-24 05:06:56.063Z | 217.748° SW |
| 9 mins | 2026-02-24 15:07:56.063Z | 128.937° SE | 2026-02-24 15:11:56.063Z | 80.025° E | 27.535° | 2026-02-24 15:16:56.063Z | 22.858° NE |
| 10 mins | 2026-02-24 16:53:56.063Z | 214.947° SW | 2026-02-24 16:57:56.063Z | 266.146° W | 32.675° | 2026-02-24 17:03:56.063Z | 342.096° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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