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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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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-5
1 60383U 24140E 25325.86827631 .00000064 00000-0 80008-4 0 9999
2 60383 88.9716 301.4449 0013233 273.0543 86.9094 13.50975896 64483Epoch: 2025-11-21T20:50Z
TLE epoch observation values (Epoch: 2025-11-21T20:50:19.073Z)
Latitude
0.00001°
Longitude
-72.2397°
Altitude
1,071.105 km
Speed
7.317 km/s
True Right ascension
20h 05m 46s
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
04:20:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.572 km
Perigee altitude
1,055.871 km
Semi-major axis
7,443.858 km
Eccentricity
0.00132
Inclination
88.9716°
RAAN
301.4449°
Arg. of periapsis
273.0543°
True anomaly
87.06083°
Mean anomaly
86.9094°
Eccentric anomaly
86.98511°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000080008
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-22 09:52:36.156Z | 20.672° NNE | 2025-11-22 09:58:36.156Z | 88.367° E | 28.71° | 2025-11-22 10:03:36.156Z | 142.625° SSE |
| 10 mins | 2025-11-22 11:40:36.156Z | 336.329° NNW | 2025-11-22 11:44:36.156Z | 283.879° WNW | 31.95° | 2025-11-22 11:50:36.156Z | 215.222° SW |
| 9 mins | 2025-11-22 21:51:36.156Z | 126.171° SE | 2025-11-22 21:55:36.156Z | 79.472° E | 26.07° | 2025-11-22 22:00:36.156Z | 24.233° NE |
| 10 mins | 2025-11-22 23:37:36.156Z | 212.009° SW | 2025-11-22 23:41:36.156Z | 265.738° W | 34.696° | 2025-11-22 23:47:36.156Z | 343.696° 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
Authenticating...
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