QIANFAN-18, 60396
Orbit data source: Space-Track
QIANFAN-18, 60396 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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60396 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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-18
1 60396U 24140T 25284.35080087 .00000029 00000-0 26902-4 0 9991
2 60396 88.9751 305.4363 0014690 17.2549 342.9099 13.50974378 59104Epoch: 2025-10-11T08:25Z
TLE epoch observation values (Epoch: 2025-10-11T08:25:09.195Z)
Latitude
0.00005°
Longitude
158.96445°
Altitude
1,061.172 km
Speed
7.326 km/s
True Right ascension
20h 21m 44s
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
14:24:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.662 km
Perigee altitude
1,054.792 km
Semi-major axis
7,443.864 km
Eccentricity
0.00147
Inclination
88.9751°
RAAN
305.4363°
Arg. of periapsis
17.2549°
True anomaly
342.86034°
Mean anomaly
342.9099°
Eccentric anomaly
342.88513°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.000026902
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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-18 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 | 2025-10-12 00:33:49.395Z | 112.723° SE | 2025-10-12 00:37:49.395Z | 70.584° E | 19.18° | 2025-10-12 00:41:49.395Z | 31.487° NE |
| 11 mins | 2025-10-12 02:18:49.395Z | 195.553° SSW | 2025-10-12 02:23:49.395Z | 288.878° WNW | 41.265° | 2025-10-12 02:29:49.395Z | 352.286° N |
| 11 mins | 2025-10-12 13:27:49.395Z | 9.693° NNE | 2025-10-12 13:32:49.395Z | 78.857° E | 42.123° | 2025-10-12 13:38:49.395Z | 169.013° S |
| 7 mins | 2025-10-12 15:15:49.395Z | 318.768° NNW | 2025-10-12 15:18:49.395Z | 286.984° WNW | 18.877° | 2025-10-12 15:22:49.395Z | 246.693° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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