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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-8
1 60386U 24140H 26171.45932546 .00000112 00000-0 15460-3 0 9992
2 60386 88.9744 279.5840 0016539 18.0385 342.1350 13.51010398 92964Epoch: 2026-06-20T11:01Z
TLE epoch observation values (Epoch: 2026-06-20T11:01:25.719Z)
Latitude
0°
Longitude
-154.44681°
Altitude
1,059.774 km
Speed
7.328 km/s
True Right ascension
18h 38m 20s
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
07:22:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.906 km
Perigee altitude
1,053.283 km
Semi-major axis
7,443.732 km
Eccentricity
0.00165
Inclination
88.9744°
RAAN
279.584°
Arg. of periapsis
18.0385°
True anomaly
342.07674°
Mean anomaly
342.135°
Eccentric anomaly
342.10588°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.0001546
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-20 20:30:55.065Z | 337.46° NNW | 2026-06-20 20:35:55.065Z | 277.452° WNW | 29.058° | 2026-06-20 20:40:55.065Z | 222.486° SW |
| 9 mins | 2026-06-21 06:42:55.065Z | 128.619° SE | 2026-06-21 06:46:55.065Z | 75.025° E | 28.599° | 2026-06-21 06:51:55.065Z | 20.386° NNE |
| 10 mins | 2026-06-21 08:28:55.065Z | 218.769° SW | 2026-06-21 08:32:55.065Z | 272.577° WNW | 31.637° | 2026-06-21 08:38:55.065Z | 342.357° N |
| 6 mins | 2026-06-21 17:52:55.065Z | 52.17° ENE | 2026-06-21 17:54:55.065Z | 71.921° E | 15.09° | 2026-06-21 17:58:55.065Z | 109.692° ESE |
| 12 mins | 2026-06-21 19:36:55.065Z | 357.81° N | 2026-06-21 19:42:55.065Z | 230.805° WSW | 44.166° | 2026-06-21 19:48:55.065Z | 187.808° SSW |
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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