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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-10
1 60388U 24140K 26171.36471350 .00000126 00000-0 17684-3 0 9990
2 60388 88.9753 279.0321 0013789 355.9583 4.1454 13.51016906 93065Epoch: 2026-06-20T08:45Z
TLE epoch observation values (Epoch: 2026-06-20T08:45:11.246Z)
Latitude
-0.00007°
Longitude
-120.84515°
Altitude
1,061.229 km
Speed
7.326 km/s
True Right ascension
18h 36m 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
08:42:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.835 km
Perigee altitude
1,055.306 km
Semi-major axis
7,443.708 km
Eccentricity
0.00138
Inclination
88.9753°
RAAN
279.0321°
Arg. of periapsis
355.9583°
True anomaly
4.15684°
Mean anomaly
4.1454°
Eccentric anomaly
4.15112°
Mean motion
3.37955 °/min
Orbital period
106.52 mins
BSTAR
0.00017684
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-21 06:13:11.585Z | 117.014° SE | 2026-06-21 06:17:11.585Z | 77.758° E | 19.269° | 2026-06-21 06:21:11.585Z | 35.704° NE |
| 11 mins | 2026-06-21 07:58:11.585Z | 193.906° SSW | 2026-06-21 08:03:11.585Z | 262.405° W | 41.458° | 2026-06-21 08:09:11.585Z | 350.979° N |
| 11 mins | 2026-06-21 19:08:11.585Z | 10.762° NNE | 2026-06-21 19:13:11.585Z | 99.522° ESE | 42.155° | 2026-06-21 19:19:11.585Z | 169.881° S |
| 7 mins | 2026-06-21 20:56:11.585Z | 315.067° NNW | 2026-06-21 20:59:11.585Z | 282.104° WNW | 18.813° | 2026-06-21 21:03:11.585Z | 243.869° WSW |
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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