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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-16
1 60394U 24140R 26171.41418553 .00000122 00000-0 16976-3 0 9998
2 60394 88.9738 279.7052 0015142 33.0321 327.1772 13.51015233 92783Epoch: 2026-06-20T09:56Z
TLE epoch observation values (Epoch: 2026-06-20T09:56:25.629Z)
Latitude
-0.00013°
Longitude
-138.03074°
Altitude
1,062.006 km
Speed
7.326 km/s
True Right ascension
18h 38m 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
08:42:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.848 km
Perigee altitude
1,054.305 km
Semi-major axis
7,443.714 km
Eccentricity
0.00151
Inclination
88.9738°
RAAN
279.7052°
Arg. of periapsis
33.0321°
True anomaly
327.083°
Mean anomaly
327.1772°
Eccentric anomaly
327.13011°
Mean motion
3.37955 °/min
Orbital period
106.52 mins
BSTAR
0.00016976
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-06-21 07:22:01.862Z | 166.309° S | 2026-06-21 07:28:01.862Z | 85.729° E | 43.004° | 2026-06-21 07:34:01.862Z | 4.934° NNE |
| 7 mins | 2026-06-21 09:12:01.862Z | 250.907° W | 2026-06-21 09:15:01.862Z | 281.855° WNW | 17.303° | 2026-06-21 09:19:01.862Z | 321.653° NNW |
| 10 mins | 2026-06-21 18:33:01.862Z | 28.486° NE | 2026-06-21 18:37:01.862Z | 76.912° E | 28.554° | 2026-06-21 18:43:01.862Z | 144.171° SSE |
| 10 mins | 2026-06-21 20:19:01.862Z | 340.16° N | 2026-06-21 20:24:01.862Z | 276.65° WNW | 32.052° | 2026-06-21 20:29:01.862Z | 217.822° SW |
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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