QIANFAN-9, 60387
Orbit data source: Space-Track
QIANFAN-9, 60387 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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60387 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-9
1 60387U 24140J 26171.43464648 .00000111 00000-0 15336-3 0 9995
2 60387 88.9742 279.6582 0016220 18.0555 342.1169 13.51015859 92946Epoch: 2026-06-20T10:25Z
TLE epoch observation values (Epoch: 2026-06-20T10:25:53.455Z)
Latitude
-0.00003°
Longitude
-145.46385°
Altitude
1,059.981 km
Speed
7.328 km/s
True Right ascension
18h 38m 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
07:22:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.648 km
Perigee altitude
1,053.501 km
Semi-major axis
7,443.711 km
Eccentricity
0.00162
Inclination
88.9742°
RAAN
279.6582°
Arg. of periapsis
18.0555°
True anomaly
342.05971°
Mean anomaly
342.1169°
Eccentric anomaly
342.08832°
Mean motion
3.37955 °/min
Orbital period
106.52 mins
BSTAR
0.00015336
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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-9 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 | 2026-06-21 06:08:19.895Z | 106.009° ESE | 2026-06-21 06:11:19.895Z | 76.504° E | 16.638° | 2026-06-21 06:15:19.895Z | 37.025° NE |
| 11 mins | 2026-06-21 07:52:19.895Z | 187.734° SSW | 2026-06-21 07:57:19.895Z | 262.701° W | 43.6° | 2026-06-21 08:03:19.895Z | 354.251° N |
| 11 mins | 2026-06-21 19:02:19.895Z | 15.206° NNE | 2026-06-21 19:07:19.895Z | 99.805° ESE | 39.471° | 2026-06-21 19:13:19.895Z | 164.735° S |
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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