QIANFAN-13, 60391
Orbit data source: Space-Track
QIANFAN-13, 60391 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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60391 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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-13
1 60391U 24140N 26171.39353045 .00000117 00000-0 16269-3 0 9995
2 60391 88.9732 279.7228 0013373 30.5664 329.6264 13.51013227 92879Epoch: 2026-06-20T09:26Z
TLE epoch observation values (Epoch: 2026-06-20T09:26:41.030Z)
Latitude
-0.00002°
Longitude
-130.55695°
Altitude
1,062.896 km
Speed
7.325 km/s
True Right ascension
18h 38m 53s
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
07:24:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.539 km
Perigee altitude
1,055.63 km
Semi-major axis
7,443.721 km
Eccentricity
0.00134
Inclination
88.9732°
RAAN
279.7228°
Arg. of periapsis
30.5664°
True anomaly
329.5488°
Mean anomaly
329.6264°
Eccentric anomaly
329.58761°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00016269
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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-13 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 | 2026-06-20 20:42:19.607Z | 336.663° NNW | 2026-06-20 20:47:19.607Z | 285.292° WNW | 24.918° | 2026-06-20 20:52:19.607Z | 230.944° WSW |
| 10 mins | 2026-06-21 06:54:19.607Z | 138.922° SSE | 2026-06-21 06:58:19.607Z | 84.511° E | 32.941° | 2026-06-21 07:04:19.607Z | 14.721° NNE |
| 9 mins | 2026-06-21 08:41:19.607Z | 229.449° WSW | 2026-06-21 08:45:19.607Z | 282.125° WNW | 27.321° | 2026-06-21 08:50:19.607Z | 336.48° NNW |
| 7 mins | 2026-06-21 18:04:19.607Z | 45.56° ENE | 2026-06-21 18:07:19.607Z | 77.572° E | 18.439° | 2026-06-21 18:11:19.607Z | 117.567° SE |
| 11 mins | 2026-06-21 19:49:19.607Z | 352.294° N | 2026-06-21 19:54:19.607Z | 277.138° WNW | 42.346° | 2026-06-21 20:00:19.607Z | 195.722° SSW |
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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