QIANFAN-10, 60388
Orbit data source: Space-Track
QIANFAN-10, 60388 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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60388 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-10
1 60388U 24140K 26118.48398977 .00000063 00000-0 79171-4 0 9997
2 60388 88.9700 284.5200 0016179 135.6059 224.6392 13.51001277 85922Epoch: 2026-04-28T11:36Z
TLE epoch observation values (Epoch: 2026-04-28T11:36:56.716Z)
Latitude
-0.00003°
Longitude
-106.17496°
Altitude
1,080.114 km
Speed
7.308 km/s
True Right ascension
18h 58m 04s
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
05:07:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.671 km
Perigee altitude
1,053.585 km
Semi-major axis
7,443.765 km
Eccentricity
0.00162
Inclination
88.97°
RAAN
284.52°
Arg. of periapsis
135.6059°
True anomaly
224.50912°
Mean anomaly
224.6392°
Eccentric anomaly
224.57414°
Mean motion
3.37951 °/min
Orbital period
106.52 mins
BSTAR
0.000079171
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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-10 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 | 2026-04-28 22:51:59.992Z | 10.177° NNE | 2026-04-28 22:57:59.992Z | 78.265° E | 39.162° | 2026-04-28 23:03:59.992Z | 162.691° S |
| 8 mins | 2026-04-29 00:40:59.992Z | 322.06° NNW | 2026-04-29 00:43:59.992Z | 288.469° WNW | 21.408° | 2026-04-29 00:48:59.992Z | 236.708° WSW |
| 10 mins | 2026-04-29 10:50:59.992Z | 146.94° SSE | 2026-04-29 10:54:59.992Z | 92.985° ESE | 36.431° | 2026-04-29 11:00:59.992Z | 12.701° NNE |
| 9 mins | 2026-04-29 12:37:59.992Z | 232.273° WSW | 2026-04-29 12:41:59.992Z | 277.553° WNW | 24.117° | 2026-04-29 12:46:59.992Z | 331.881° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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