QIANFAN-6, 60384
Orbit data source: Space-Track
QIANFAN-6, 60384 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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60384 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: 5 hours ago
TLE from 5 hours ago
0 QIANFAN-6
1 60384U 24140F 25285.00521580 .00000030 00000-0 28490-4 0 9995
2 60384 88.9750 305.4243 0013734 23.0859 337.0906 13.50972685 59161Epoch: 2025-10-12T00:07Z
TLE epoch observation values (Epoch: 2025-10-12T00:07:30.645Z)
Latitude
-0.00005°
Longitude
-77.28195°
Altitude
1,062.215 km
Speed
7.325 km/s
True Right ascension
20h 21m 41s
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
23:17:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.957 km
Perigee altitude
1,055.51 km
Semi-major axis
7,443.87 km
Eccentricity
0.00137
Inclination
88.975°
RAAN
305.4243°
Arg. of periapsis
23.0859°
True anomaly
337.02924°
Mean anomaly
337.0906°
Eccentric anomaly
337.05993°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00002849
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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-6 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-12 13:09:18.963Z | 13.229° NNE | 2025-10-12 13:15:18.963Z | 82.342° E | 36.331° | 2025-10-12 13:21:18.963Z | 157.406° SSE |
| 9 mins | 2025-10-12 14:57:18.963Z | 331.411° NNW | 2025-10-12 15:01:18.963Z | 287.76° WNW | 24.58° | 2025-10-12 15:06:18.963Z | 232.396° WSW |
| 10 mins | 2025-10-13 01:08:18.963Z | 140.581° SSE | 2025-10-13 01:12:18.963Z | 88.592° E | 33.164° | 2025-10-13 01:18:18.963Z | 15.111° NNE |
| 9 mins | 2025-10-13 02:55:18.963Z | 228.516° WSW | 2025-10-13 02:59:18.963Z | 279.043° WNW | 27.048° | 2025-10-13 03:04:18.963Z | 335.167° NNW |
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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