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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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-2
1 60380U 24140B 26171.39765708 .00000133 00000-0 18715-3 0 9992
2 60380 88.9723 279.4099 0012337 9.9137 350.2256 13.51010931 93011Epoch: 2026-06-20T09:32Z
TLE epoch observation values (Epoch: 2026-06-20T09:32:37.571Z)
Latitude
0.00004°
Longitude
-132.35951°
Altitude
1,062.439 km
Speed
7.325 km/s
True Right ascension
18h 37m 38s
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
07:24:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.776 km
Perigee altitude
1,056.409 km
Semi-major axis
7,443.73 km
Eccentricity
0.00123
Inclination
88.9723°
RAAN
279.4099°
Arg. of periapsis
9.9137°
True anomaly
350.20156°
Mean anomaly
350.2256°
Eccentric anomaly
350.21359°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00018715
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-20 20:48:39.434Z | 332.547° NNW | 2026-06-20 20:53:39.434Z | 280.074° WNW | 22.451° | 2026-06-20 20:57:39.434Z | 238.314° WSW |
| 10 mins | 2026-06-21 06:59:39.434Z | 146.976° SSE | 2026-06-21 07:04:39.434Z | 74.795° E | 35.628° | 2026-06-21 07:09:39.434Z | 14.605° NNE |
| 9 mins | 2026-06-21 08:46:39.434Z | 228.805° WSW | 2026-06-21 08:50:39.434Z | 272.697° WNW | 24.646° | 2026-06-21 08:55:39.434Z | 330.553° NNW |
| 8 mins | 2026-06-21 18:09:39.434Z | 38.382° NE | 2026-06-21 18:13:39.434Z | 82.248° E | 20.724° | 2026-06-21 18:17:39.434Z | 123.136° SE |
| 11 mins | 2026-06-21 19:55:39.434Z | 347.943° N | 2026-06-21 20:00:39.434Z | 262.77° W | 40.029° | 2026-06-21 20:06:39.434Z | 199.637° SSW |
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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