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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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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-6
1 60384U 24140F 26113.90433089 .00000052 00000-0 61304-4 0 9996
2 60384 88.9687 285.3245 0013645 166.3240 193.8284 13.51005852 85344Epoch: 2026-04-23T21:42Z
TLE epoch observation values (Epoch: 2026-04-23T21:42:14.188Z)
Latitude
0°
Longitude
107.82067°
Altitude
1,081.383 km
Speed
7.307 km/s
True Right ascension
19h 01m 17s
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
11:11:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.768 km
Perigee altitude
1,055.454 km
Semi-major axis
7,443.748 km
Eccentricity
0.00136
Inclination
88.9687°
RAAN
285.3245°
Arg. of periapsis
166.324°
True anomaly
193.79109°
Mean anomaly
193.8284°
Eccentric anomaly
193.80974°
Mean motion
3.37952 °/min
Orbital period
106.52 mins
BSTAR
0.000061304
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-04-24 10:17:28.776Z | 110.646° ESE | 2026-04-24 10:21:28.776Z | 72.884° E | 16.695° | 2026-04-24 10:25:28.776Z | 34.972° NE |
| 11 mins | 2026-04-24 12:02:28.776Z | 187.613° SSW | 2026-04-24 12:07:28.776Z | 287.972° WNW | 43.724° | 2026-04-24 12:13:28.776Z | 355.012° N |
| 11 mins | 2026-04-24 23:11:28.776Z | 12.992° NNE | 2026-04-24 23:16:28.776Z | 76.09° E | 39.068° | 2026-04-24 23:22:28.776Z | 162.4° S |
| 8 mins | 2026-04-25 00:59:28.776Z | 322.621° NNW | 2026-04-25 01:02:28.776Z | 289.332° WNW | 21.475° | 2026-04-25 01:07:28.776Z | 237.071° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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