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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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: 2 days ago
TLE from 2 days ago
0 QIANFAN-4
1 60382U 24140D 25312.78345306 .00000048 00000-0 55914-4 0 9999
2 60382 88.9733 302.6695 0011184 292.2172 67.7792 13.50977112 62855Epoch: 2025-11-08T18:48Z
TLE epoch observation values (Epoch: 2025-11-08T18:48:10.344Z)
Latitude
-0.00005°
Longitude
-27.58171°
Altitude
1,068.477 km
Speed
7.319 km/s
True Right ascension
20h 10m 40s
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
06:52:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.042 km
Perigee altitude
1,057.392 km
Semi-major axis
7,443.854 km
Eccentricity
0.00112
Inclination
88.9733°
RAAN
302.6695°
Arg. of periapsis
292.2172°
True anomaly
67.8979°
Mean anomaly
67.7792°
Eccentric anomaly
67.83855°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000055914
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-10 10:34:05.327Z | 57.357° ENE | 2025-11-10 10:36:05.327Z | 84.692° E | 23.704° | 2025-11-10 10:41:05.327Z | 134.515° SE |
| 10 mins | 2025-11-10 12:18:05.327Z | 343.232° N | 2025-11-10 12:22:05.327Z | 290.385° WNW | 36.899° | 2025-11-10 12:28:05.327Z | 207.446° SW |
| 8 mins | 2025-11-10 22:30:05.327Z | 113.54° SE | 2025-11-10 22:33:05.327Z | 81.189° E | 21.132° | 2025-11-10 22:38:05.327Z | 29.113° NE |
| 10 mins | 2025-11-11 00:15:05.327Z | 200.738° SSW | 2025-11-11 00:19:05.327Z | 255.627° W | 39.467° | 2025-11-11 00:25:05.327Z | 348.167° N |
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
Authenticating...
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