QIANFAN-2, 60380
Orbit data source: Space-Track
QIANFAN-2, 60380 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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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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-2
1 60380U 24140B 25326.35387682 .00000054 00000-0 64921-4 0 9993
2 60380 88.9724 301.2347 0010877 243.5836 116.4199 13.50972308 64651Epoch: 2025-11-22T08:29Z
TLE epoch observation values (Epoch: 2025-11-22T08:29:34.957Z)
Latitude
-0.00004°
Longitude
112.25528°
Altitude
1,075.248 km
Speed
7.313 km/s
True Right ascension
20h 04m 56s
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
14:20:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.831 km
Perigee altitude
1,057.638 km
Semi-major axis
7,443.872 km
Eccentricity
0.00109
Inclination
88.9724°
RAAN
301.2347°
Arg. of periapsis
243.5836°
True anomaly
116.53146°
Mean anomaly
116.4199°
Eccentric anomaly
116.47568°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.000064921
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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-2 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 | 2025-11-22 21:07:25.206Z | 85.77° E | 2025-11-22 21:09:25.206Z | 67.407° ENE | 11.952° | 2025-11-22 21:11:25.206Z | 49.43° ENE |
| 11 mins | 2025-11-22 22:49:25.206Z | 173.313° S | 2025-11-22 22:54:25.206Z | 122.842° SE | 44.68° | 2025-11-22 23:00:25.206Z | 1.131° NNE |
| 5 mins | 2025-11-23 00:40:25.206Z | 269.805° W | 2025-11-23 00:42:25.206Z | 289.861° WNW | 14.369° | 2025-11-23 00:45:25.206Z | 317.296° NNW |
| 10 mins | 2025-11-23 09:59:25.206Z | 22.131° NNE | 2025-11-23 10:04:25.206Z | 89.654° E | 32.775° | 2025-11-23 10:09:25.206Z | 148.988° SSE |
| 9 mins | 2025-11-23 11:46:25.206Z | 332.254° NNW | 2025-11-23 11:50:25.206Z | 283.236° WNW | 27.875° | 2025-11-23 11:55:25.206Z | 225.843° 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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