QIANFAN-5, 60383
Orbit data source: Space-Track
QIANFAN-5, 60383 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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60383 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-5
1 60383U 24140E 26054.11484425 .00000094 00000-0 12746-3 0 9993
2 60383 88.9712 291.7800 0015674 8.5055 351.6359 13.51000118 77073Epoch: 2026-02-23T02:45Z
TLE epoch observation values (Epoch: 2026-02-23T02:45:22.543Z)
Latitude
0.00001°
Longitude
97.42271°
Altitude
1,059.985 km
Speed
7.328 km/s
True Right ascension
19h 27m 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
12:54:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.3 km
Perigee altitude
1,053.965 km
Semi-major axis
7,443.769 km
Eccentricity
0.00157
Inclination
88.9712°
RAAN
291.78°
Arg. of periapsis
8.5055°
True anomaly
351.60972°
Mean anomaly
351.6359°
Eccentric anomaly
351.62282°
Mean motion
3.37951 °/min
Orbital period
106.52 mins
BSTAR
0.00012746
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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-5 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-02-23 15:18:54.628Z | 139.624° SSE | 2026-02-23 15:23:54.628Z | 81.514° E | 30.391° | 2026-02-23 15:28:54.628Z | 20.712° NNE |
| 10 mins | 2026-02-23 17:05:54.628Z | 219.354° SW | 2026-02-23 17:10:54.628Z | 285.027° WNW | 29.723° | 2026-02-23 17:15:54.628Z | 339.263° N |
| 6 mins | 2026-02-24 02:29:54.628Z | 47.95° ENE | 2026-02-24 02:32:54.628Z | 78.586° E | 16.472° | 2026-02-24 02:35:54.628Z | 108.152° ESE |
| 11 mins | 2026-02-24 04:14:54.628Z | 355.159° N | 2026-02-24 04:19:54.628Z | 270.853° WNW | 43.844° | 2026-02-24 04:25:54.628Z | 191.142° SSW |
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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