QIANFAN-7, 60385
Orbit data source: Space-Track
QIANFAN-7, 60385 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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60385 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Partially 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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-7
1 60385U 24140G 26171.46313036 .00000427 00000-0 16638-3 0 9996
2 60385 88.9776 271.3888 0017274 131.5940 228.6738 14.27841492 97464Epoch: 2026-06-20T11:06Z
TLE epoch observation values (Epoch: 2026-06-20T11:06:54.463Z)
Latitude
-0.00002°
Longitude
-164.01552°
Altitude
810.22 km
Speed
7.444 km/s
True Right ascension
18h 05m 33s
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
10:18:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
808.287 km
Perigee altitude
783.503 km
Semi-major axis
7,174.032 km
Eccentricity
0.00173
Inclination
88.9776°
RAAN
271.3888°
Arg. of periapsis
131.594°
True anomaly
228.52536°
Mean anomaly
228.6738°
Eccentric anomaly
228.59956°
Mean motion
3.57189 °/min
Orbital period
100.79 mins
BSTAR
0.00016638
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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-7 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 05:46:23.394Z | 103.913° ESE | 2026-06-21 05:48:23.394Z | 80.268° E | 14.617° | 2026-06-21 05:51:23.394Z | 43.988° NE |
| 8 mins | 2026-06-21 07:25:23.394Z | 195.182° SSW | 2026-06-21 07:29:23.394Z | 289.502° WNW | 40.83° | 2026-06-21 07:33:23.394Z | 349.515° N |
| 7 mins | 2026-06-21 17:59:23.394Z | 37.876° NE | 2026-06-21 18:02:23.394Z | 81.838° E | 22.533° | 2026-06-21 18:06:23.394Z | 134.554° SE |
| 7 mins | 2026-06-21 19:40:23.394Z | 331.136° NNW | 2026-06-21 19:43:23.394Z | 275.965° WNW | 30.431° | 2026-06-21 19:47:23.394Z | 216.702° SW |
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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