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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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 26171.42634255 .00000107 00000-0 14642-3 0 9998
2 60393 88.9735 279.5785 0012309 17.4159 342.7412 13.51007403 92871Epoch: 2026-06-20T10:13Z
TLE epoch observation values (Epoch: 2026-06-20T10:13:55.996Z)
Latitude
-0°
Longitude
-142.54595°
Altitude
1,062.753 km
Speed
7.325 km/s
True Right ascension
18h 38m 18s
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
07:23:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.768 km
Perigee altitude
1,056.443 km
Semi-major axis
7,443.743 km
Eccentricity
0.00123
Inclination
88.9735°
RAAN
279.5785°
Arg. of periapsis
17.4159°
True anomaly
342.69929°
Mean anomaly
342.7412°
Eccentric anomaly
342.72025°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.00014642
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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
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-21 05:58:00.977Z | 89.333° E | 2026-06-21 06:00:00.977Z | 69.948° E | 13.513° | 2026-06-21 06:02:00.977Z | 50.739° ENE |
| 12 mins | 2026-06-21 07:40:00.977Z | 178.601° S | 2026-06-21 07:45:00.977Z | 189.935° SSW | 44.409° | 2026-06-21 07:52:00.977Z | 358.737° N |
| 11 mins | 2026-06-21 18:50:00.977Z | 18.444° NNE | 2026-06-21 18:55:00.977Z | 85.702° E | 35.528° | 2026-06-21 19:01:00.977Z | 156.468° SSE |
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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