QIANFAN-14, 60392
Orbit data source: Space-Track
QIANFAN-14, 60392 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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60392 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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-14
1 60392U 24140P 26054.62085992 .00000090 00000-0 12073-3 0 9994
2 60392 88.9707 291.7590 0017003 3.7908 356.3369 13.50999362 77110Epoch: 2026-02-23T14:54Z
TLE epoch observation values (Epoch: 2026-02-23T14:54:02.297Z)
Latitude
0.00002°
Longitude
-85.26269°
Altitude
1,058.899 km
Speed
7.329 km/s
True Right ascension
19h 27m 02s
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
02:06:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.292 km
Perigee altitude
1,052.978 km
Semi-major axis
7,443.772 km
Eccentricity
0.0017
Inclination
88.9707°
RAAN
291.759°
Arg. of periapsis
3.7908°
True anomaly
356.32443°
Mean anomaly
356.3369°
Eccentric anomaly
356.33067°
Mean motion
3.37951 °/min
Orbital period
106.52 mins
BSTAR
0.00012073
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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-14 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 | 2026-02-24 02:12:31.152Z | 55.004° ENE | 2026-02-24 02:14:31.152Z | 73.058° E | 11.595° | 2026-02-24 02:16:31.152Z | 91.071° ESE |
| 12 mins | 2026-02-24 03:56:31.152Z | 3.242° NNE | 2026-02-24 04:02:31.152Z | 148.157° SSE | 44.199° | 2026-02-24 04:08:31.152Z | 179.233° S |
| 5 mins | 2026-02-24 05:45:31.152Z | 309.637° NW | 2026-02-24 05:47:31.152Z | 289.953° WNW | 14.831° | 2026-02-24 05:50:31.152Z | 261.157° W |
| 11 mins | 2026-02-24 15:53:31.152Z | 167.507° S | 2026-02-24 15:58:31.152Z | 115.364° SE | 43.206° | 2026-02-24 16:04:31.152Z | 4.426° NNE |
| 6 mins | 2026-02-24 17:43:31.152Z | 256.777° W | 2026-02-24 17:46:31.152Z | 288.173° WNW | 16.41° | 2026-02-24 17:49:31.152Z | 317.577° NNW |
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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