QIANFAN-16, 60394
Orbit data source: Space-Track
QIANFAN-16, 60394 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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60394 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: 1 day ago
TLE from 1 day ago
0 QIANFAN-16
1 60394U 24140R 25312.81648247 .00000032 00000-0 31539-4 0 9996
2 60394 88.9730 302.9057 0013235 316.6403 43.3705 13.50972857 62593Epoch: 2025-11-08T19:35Z
TLE epoch observation values (Epoch: 2025-11-08T19:35:44.085Z)
Latitude
-0.00011°
Longitude
-39.26865°
Altitude
1,064.475 km
Speed
7.323 km/s
True Right ascension
20h 11m 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
18:58:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.585 km
Perigee altitude
1,055.881 km
Semi-major axis
7,443.87 km
Eccentricity
0.00132
Inclination
88.973°
RAAN
302.9057°
Arg. of periapsis
316.6403°
True anomaly
43.47477°
Mean anomaly
43.3705°
Eccentric anomaly
43.42262°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.000031539
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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-16 Visibility forecast
Loading observer location...
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 | 2025-11-10 00:07:45.777Z | 188.163° SSW | 2025-11-10 00:13:45.777Z | 259.089° W | 42.881° | 2025-11-10 00:19:45.777Z | 352.899° N |
| 11 mins | 2025-11-10 11:18:45.777Z | 13.004° NNE | 2025-11-10 11:23:45.777Z | 94.271° ESE | 40.71° | 2025-11-10 11:29:45.777Z | 166.372° S |
| 8 mins | 2025-11-10 13:05:45.777Z | 325.329° NNW | 2025-11-10 13:09:45.777Z | 282.829° WNW | 20.509° | 2025-11-10 13:13:45.777Z | 242.335° 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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