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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-10
1 60388U 24140K 26054.64136210 .00000091 00000-0 12229-3 0 9995
2 60388 88.9746 291.1578 0014068 331.2654 28.7721 13.51001825 77305Epoch: 2026-02-23T15:23Z
TLE epoch observation values (Epoch: 2026-02-23T15:23:33.685Z)
Latitude
0.00001°
Longitude
-93.26488°
Altitude
1,062.347 km
Speed
7.325 km/s
True Right ascension
19h 24m 37s
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
02:00:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.098 km
Perigee altitude
1,055.154 km
Semi-major axis
7,443.763 km
Eccentricity
0.00141
Inclination
88.9746°
RAAN
291.1578°
Arg. of periapsis
331.2654°
True anomaly
28.84981°
Mean anomaly
28.7721°
Eccentric anomaly
28.81094°
Mean motion
3.37951 °/min
Orbital period
106.52 mins
BSTAR
0.00012229
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-02-24 02:39:56.311Z | 31.772° NE | 2026-02-24 02:44:56.311Z | 83.414° E | 20.754° | 2026-02-24 02:48:56.311Z | 123.761° SE |
| 11 mins | 2026-02-24 04:26:56.311Z | 347.604° N | 2026-02-24 04:31:56.311Z | 259.526° W | 39.922° | 2026-02-24 04:37:56.311Z | 199.47° SSW |
| 7 mins | 2026-02-24 14:39:56.311Z | 102.285° ESE | 2026-02-24 14:42:56.311Z | 69.494° E | 18.304° | 2026-02-24 14:46:56.311Z | 31.596° NE |
| 12 mins | 2026-02-24 16:22:56.311Z | 190.785° SSW | 2026-02-24 16:28:56.311Z | 296.454° NW | 41.943° | 2026-02-24 16:34:56.311Z | 353.455° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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