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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-14
1 60392U 24140P 26171.41818226 .00000125 00000-0 17493-3 0 9995
2 60392 88.9711 279.5777 0017013 28.2161 331.9908 13.51006824 92882Epoch: 2026-06-20T10:02Z
TLE epoch observation values (Epoch: 2026-06-20T10:02:10.947Z)
Latitude
-0.00003°
Longitude
-139.60101°
Altitude
1,060.327 km
Speed
7.327 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
07:22:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.272 km
Perigee altitude
1,052.944 km
Semi-major axis
7,443.745 km
Eccentricity
0.0017
Inclination
88.9711°
RAAN
279.5777°
Arg. of periapsis
28.2161°
True anomaly
331.89907°
Mean anomaly
331.9908°
Eccentric anomaly
331.94495°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.00017493
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 21:19:13.457Z | 318.288° NNW | 2026-06-20 21:22:13.457Z | 290.833° WNW | 13.841° | 2026-06-20 21:25:13.457Z | 262.688° W |
| 11 mins | 2026-06-21 07:29:13.457Z | 168.9° S | 2026-06-21 07:34:13.457Z | 47.722° ENE | 43.728° | 2026-06-21 07:40:13.457Z | 2.453° NNE |
| 6 mins | 2026-06-21 09:18:13.457Z | 256.582° W | 2026-06-21 09:21:13.457Z | 286.741° WNW | 15.433° | 2026-06-21 09:24:13.457Z | 315.877° NNW |
| 10 mins | 2026-06-21 18:38:13.457Z | 22.749° NE | 2026-06-21 18:43:13.457Z | 84.827° E | 31.046° | 2026-06-21 18:48:13.457Z | 144.922° SSE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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