QIANFAN-4, 60382
Orbit data source: Space-Track
QIANFAN-4, 60382 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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60382 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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-4
1 60382U 24140D 26171.38115646 .00000113 00000-0 15586-3 0 9994
2 60382 88.9741 279.4753 0012675 12.4486 347.6976 13.51014674 93041Epoch: 2026-06-20T09:08Z
TLE epoch observation values (Epoch: 2026-06-20T09:08:51.918Z)
Latitude
0.00002°
Longitude
-126.33762°
Altitude
1,062.258 km
Speed
7.325 km/s
True Right ascension
18h 37m 54s
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
08:41:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.014 km
Perigee altitude
1,056.144 km
Semi-major axis
7,443.716 km
Eccentricity
0.00127
Inclination
88.9741°
RAAN
279.4753°
Arg. of periapsis
12.4486°
True anomaly
347.6666°
Mean anomaly
347.6976°
Eccentric anomaly
347.68211°
Mean motion
3.37955 °/min
Orbital period
106.52 mins
BSTAR
0.00015586
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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-4 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 | 2026-06-21 06:35:42.947Z | 133.89° SE | 2026-06-21 06:40:42.947Z | 80.261° E | 26.672° | 2026-06-21 06:45:42.947Z | 23.672° NE |
| 10 mins | 2026-06-21 08:22:42.947Z | 213.291° SW | 2026-06-21 08:26:42.947Z | 265.252° W | 33.561° | 2026-06-21 08:32:42.947Z | 342.812° N |
| 4 mins | 2026-06-21 17:47:42.947Z | 59.31° ENE | 2026-06-21 17:49:42.947Z | 78.865° E | 13.544° | 2026-06-21 17:51:42.947Z | 97.595° ESE |
| 11 mins | 2026-06-21 19:31:42.947Z | 359.923° N | 2026-06-21 19:36:42.947Z | 239.632° WSW | 44.941° | 2026-06-21 19:42:42.947Z | 184.336° SSW |
| 4 mins | 2026-06-21 21:20:42.947Z | 303.244° NW | 2026-06-21 21:21:42.947Z | 293.84° NW | 12.617° | 2026-06-21 21:24:42.947Z | 266.299° W |
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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