QIANFAN-9, 60387
Orbit data source: Space-Track
QIANFAN-9, 60387 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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60387 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-9
1 60387U 24140J 25284.98870926 .00000051 00000-0 60993-4 0 9992
2 60387 88.9751 305.7390 0016922 23.3900 336.8017 13.50973525 58997Epoch: 2025-10-11T23:43Z
TLE epoch observation values (Epoch: 2025-10-11T23:43:44.480Z)
Latitude
-0.00003°
Longitude
-71.00863°
Altitude
1,060.05 km
Speed
7.328 km/s
True Right ascension
20h 22m 57s
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
04:07:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.327 km
Perigee altitude
1,053.134 km
Semi-major axis
7,443.867 km
Eccentricity
0.00169
Inclination
88.9751°
RAAN
305.739°
Arg. of periapsis
23.39°
True anomaly
336.72517°
Mean anomaly
336.8017°
Eccentric anomaly
336.76345°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.000060993
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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-9 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 | 2025-10-12 12:46:20.028Z | 24.536° NE | 2025-10-12 12:51:20.028Z | 78.939° E | 26.906° | 2025-10-12 12:56:20.028Z | 136.758° SSE |
| 10 mins | 2025-10-12 14:33:20.028Z | 341.416° N | 2025-10-12 14:38:20.028Z | 274.108° WNW | 33.843° | 2025-10-12 14:43:20.028Z | 214.529° SW |
| 9 mins | 2025-10-13 00:45:20.028Z | 121.322° SE | 2025-10-13 00:49:20.028Z | 74.177° E | 24.016° | 2025-10-13 00:54:20.028Z | 23.533° NE |
| 11 mins | 2025-10-13 02:30:20.028Z | 205.207° SW | 2025-10-13 02:35:20.028Z | 274.118° WNW | 36.55° | 2025-10-13 02:41:20.028Z | 346.737° N |
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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