QIANFAN-15, 60393
Orbit data source: Space-Track
QIANFAN-15, 60393 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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60393 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-15
1 60393U 24140Q 25325.86405828 .00000064 00000-0 80157-4 0 9995
2 60393 88.9735 301.4320 0010466 253.7714 106.2286 13.50974107 64442Epoch: 2025-11-21T20:44Z
TLE epoch observation values (Epoch: 2025-11-21T20:44:14.635Z)
Latitude
-0°
Longitude
-70.72995°
Altitude
1,073.816 km
Speed
7.314 km/s
True Right ascension
20h 05m 43s
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
04:18:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.519 km
Perigee altitude
1,057.937 km
Semi-major axis
7,443.865 km
Eccentricity
0.00105
Inclination
88.9735°
RAAN
301.432°
Arg. of periapsis
253.7714°
True anomaly
106.34371°
Mean anomaly
106.2286°
Eccentric anomaly
106.28616°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000080157
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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-15 Visibility forecast
Loading observer location...
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 | 2025-11-22 09:46:53.896Z | 24.38° NE | 2025-11-22 09:51:53.896Z | 77.699° E | 26.488° | 2025-11-22 09:56:53.896Z | 135.79° SSE |
| 11 mins | 2025-11-22 11:33:53.896Z | 342.166° N | 2025-11-22 11:38:53.896Z | 275.865° WNW | 34.209° | 2025-11-22 11:44:53.896Z | 210.456° SW |
| 9 mins | 2025-11-22 21:45:53.896Z | 120.675° SE | 2025-11-22 21:49:53.896Z | 74.22° E | 23.97° | 2025-11-22 21:54:53.896Z | 23.942° NE |
| 11 mins | 2025-11-22 23:30:53.896Z | 204.582° SW | 2025-11-22 23:35:53.896Z | 274.189° WNW | 37.13° | 2025-11-22 23:41:53.896Z | 346.987° 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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