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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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: 5 hours ago
TLE from 5 hours ago
0 QIANFAN-18
1 60396U 24140T 26114.50916159 .00000054 00000-0 65271-4 0 9999
2 60396 88.9688 285.2053 0015078 158.3393 201.8399 13.51007839 85452Epoch: 2026-04-24T12:13Z
TLE epoch observation values (Epoch: 2026-04-24T12:13:11.561Z)
Latitude
-0.00002°
Longitude
-110.63374°
Altitude
1,081.933 km
Speed
7.306 km/s
True Right ascension
19h 00m 49s
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
00:38:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.828 km
Perigee altitude
1,054.38 km
Semi-major axis
7,443.741 km
Eccentricity
0.00151
Inclination
88.9688°
RAAN
285.2053°
Arg. of periapsis
158.3393°
True anomaly
201.77574°
Mean anomaly
201.8399°
Eccentric anomaly
201.80781°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.000065271
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-04-24 23:28:58.613Z | 5.303° NNE | 2026-04-24 23:34:58.613Z | 123.434° SE | 43.661° | 2026-04-24 23:40:58.613Z | 175.694° S |
| 6 mins | 2026-04-25 01:17:58.613Z | 311.49° NW | 2026-04-25 01:19:58.613Z | 291.067° WNW | 15.978° | 2026-04-25 01:23:58.613Z | 252.302° W |
| 12 mins | 2026-04-25 11:25:58.613Z | 163.791° S | 2026-04-25 11:31:58.613Z | 62.589° ENE | 42.025° | 2026-04-25 11:37:58.613Z | 5.21° NNE |
| 7 mins | 2026-04-25 13:15:58.613Z | 254.281° W | 2026-04-25 13:18:58.613Z | 287.1° WNW | 18.279° | 2026-04-25 13:22:58.613Z | 325.442° NNW |
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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