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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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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-10
1 60388U 24140K 25326.46903531 .00000051 00000-0 60496-4 0 9990
2 60388 88.9753 300.7812 0012996 229.8219 130.1795 13.50978443 64727Epoch: 2025-11-22T11:15Z
TLE epoch observation values (Epoch: 2025-11-22T11:15:24.650Z)
Latitude
-0.00004°
Longitude
70.23122°
Altitude
1,077.866 km
Speed
7.31 km/s
True Right ascension
20h 03m 07s
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
21:04:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.386 km
Perigee altitude
1,056.038 km
Semi-major axis
7,443.849 km
Eccentricity
0.0013
Inclination
88.9753°
RAAN
300.7812°
Arg. of periapsis
229.8219°
True anomaly
130.29316°
Mean anomaly
130.1795°
Eccentric anomaly
130.23634°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.000060496
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-23 09:12:59.952Z | 43.734° NE | 2025-11-23 09:15:59.952Z | 73.751° E | 16.895° | 2025-11-23 09:19:59.952Z | 113.323° SE |
| 11 mins | 2025-11-23 10:57:59.952Z | 354.964° N | 2025-11-23 11:02:59.952Z | 300.156° NW | 43.11° | 2025-11-23 11:08:59.952Z | 192.953° SSW |
| 5 mins | 2025-11-23 21:12:59.952Z | 88.163° E | 2025-11-23 21:14:59.952Z | 67.818° E | 15.051° | 2025-11-23 21:17:59.952Z | 40.02° NE |
| 11 mins | 2025-11-23 22:54:59.952Z | 182.275° SSW | 2025-11-23 22:59:59.952Z | 231.978° WSW | 44.49° | 2025-11-23 23:05:59.952Z | 356.559° N |
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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