QIANFAN-3, 60381
Orbit data source: Space-Track
QIANFAN-3, 60381 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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60381 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: 22 hours ago
TLE from 22 hours ago
0 QIANFAN-3
1 60381U 24140C 25312.80827295 .00000041 00000-0 44387-4 0 9998
2 60381 88.9708 302.7779 0012273 303.1930 56.8044 13.50976713 62736Epoch: 2025-11-08T19:23Z
TLE epoch observation values (Epoch: 2025-11-08T19:23:54.782Z)
Latitude
-0.00001°
Longitude
-36.43293°
Altitude
1,066.623 km
Speed
7.321 km/s
True Right ascension
20h 11m 06s
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
13:49:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.854 km
Perigee altitude
1,056.583 km
Semi-major axis
7,443.855 km
Eccentricity
0.00123
Inclination
88.9708°
RAAN
302.7779°
Arg. of periapsis
303.193°
True anomaly
56.92219°
Mean anomaly
56.8044°
Eccentric anomaly
56.86328°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000044387
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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-3 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 | 2025-11-09 22:13:43.552Z | 98.118° ESE | 2025-11-09 22:16:43.552Z | 69.198° E | 14.61° | 2025-11-09 22:19:43.552Z | 41.237° NE |
| 12 mins | 2025-11-09 23:56:43.552Z | 181.208° SSW | 2025-11-10 00:01:43.552Z | 214.638° SW | 44.383° | 2025-11-10 00:08:43.552Z | 357.669° N |
| 11 mins | 2025-11-10 11:06:43.552Z | 16.95° NNE | 2025-11-10 11:11:43.552Z | 85.247° E | 36.894° | 2025-11-10 11:17:43.552Z | 158.597° S |
| 9 mins | 2025-11-10 12:53:43.552Z | 330.217° NNW | 2025-11-10 12:57:43.552Z | 286.09° WNW | 24.23° | 2025-11-10 13:02:43.552Z | 232.399° WSW |
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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