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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-7
1 60385U 24140G 26054.21458065 .00000393 00000-0 15298-3 0 9994
2 60385 88.9748 285.2150 0015455 154.7842 205.4110 14.27764672 80739Epoch: 2026-02-23T05:08Z
TLE epoch observation values (Epoch: 2026-02-23T05:08:59.768Z)
Latitude
-0.00002°
Longitude
54.8543°
Altitude
812.301 km
Speed
7.442 km/s
True Right ascension
19h 00m 51s
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
16:17:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
807.24 km
Perigee altitude
785.065 km
Semi-major axis
7,174.29 km
Eccentricity
0.00155
Inclination
88.9748°
RAAN
285.215°
Arg. of periapsis
154.7842°
True anomaly
205.33514°
Mean anomaly
205.411°
Eccentric anomaly
205.37306°
Mean motion
3.5717 °/min
Orbital period
100.79 mins
BSTAR
0.00015298
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-02-23 15:21:39.261Z | 156.373° SSE | 2026-02-23 15:25:39.261Z | 90.348° ESE | 38.481° | 2026-02-23 15:30:39.261Z | 9.916° NNE |
| 5 mins | 2026-02-23 17:04:39.261Z | 250.933° W | 2026-02-23 17:06:39.261Z | 276.51° WNW | 16.711° | 2026-02-23 17:09:39.261Z | 314.844° NW |
| 8 mins | 2026-02-24 03:36:39.261Z | 1.899° NNE | 2026-02-24 03:40:39.261Z | 174.089° S | 44.06° | 2026-02-24 03:44:39.261Z | 181.447° SSW |
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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