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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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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-16
1 60394U 24140R 26054.46858331 .00000105 00000-0 14430-3 0 9999
2 60394 88.9734 291.8709 0015075 8.8715 351.2700 13.51003192 76990Epoch: 2026-02-23T11:14Z
TLE epoch observation values (Epoch: 2026-02-23T11:14:45.597Z)
Latitude
-0.00002°
Longitude
-30.18111°
Altitude
1,060.425 km
Speed
7.327 km/s
True Right ascension
19h 27m 29s
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
20:21:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.842 km
Perigee altitude
1,054.4 km
Semi-major axis
7,443.758 km
Eccentricity
0.00151
Inclination
88.9734°
RAAN
291.8709°
Arg. of periapsis
8.8715°
True anomaly
351.24373°
Mean anomaly
351.27°
Eccentric anomaly
351.25687°
Mean motion
3.37952 °/min
Orbital period
106.52 mins
BSTAR
0.0001443
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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
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-02-24 03:49:41.630Z | 4.7° NNE | 2026-02-24 03:55:41.630Z | 62.637° ENE | 43.643° | 2026-02-24 04:02:41.630Z | 175.333° S |
| 6 mins | 2026-02-24 05:39:41.630Z | 309.337° NW | 2026-02-24 05:41:41.630Z | 288.477° WNW | 16.6° | 2026-02-24 05:45:41.630Z | 250.399° W |
| 11 mins | 2026-02-24 15:47:41.630Z | 162.682° S | 2026-02-24 15:52:41.630Z | 100.168° ESE | 41.935° | 2026-02-24 15:58:41.630Z | 6.632° NNE |
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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