QIANFAN-105, 66047
Orbit data source: Space-Track
QIANFAN-105, 66047 is a Chinese payload satellite in LEO that was launched on Fri, 17 Oct 2025 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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66047 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, 14.5 m
Radar Cross Section
13.200 m²
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-105
1 66047U 25233Q 26130.20073145 .00000130 00000-0 18203-3 0 9993
2 66047 89.0044 46.7675 0002239 69.5597 290.5794 13.51005160 28213Epoch: 2026-05-10T04:49Z
TLE epoch observation values (Epoch: 2026-05-10T04:49:03.197Z)
Latitude
-0.00005°
Longitude
106.49696°
Altitude
1,070.93 km
Speed
7.317 km/s
True Right ascension
03h 07m 04s
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
19:44:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.28 km
Perigee altitude
1,063.947 km
Semi-major axis
7,443.751 km
Eccentricity
0.00022
Inclination
89.0044°
RAAN
46.7675°
Arg. of periapsis
69.5597°
True anomaly
290.55538°
Mean anomaly
290.5794°
Eccentric anomaly
290.56739°
Mean motion
3.37952 °/min
Orbital period
106.52 mins
BSTAR
0.00018203
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Other satellites on launch #233 in the year 2025 (2025-10-17 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-105 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-10 17:24:45.345Z | 108.761° ESE | 2026-05-10 17:27:45.345Z | 78.692° E | 18.052° | 2026-05-10 17:31:45.345Z | 37.432° NE |
| 11 mins | 2026-05-10 19:08:45.345Z | 190.653° SSW | 2026-05-10 19:13:45.345Z | 255.2° W | 42.496° | 2026-05-10 19:19:45.345Z | 352.246° N |
| 11 mins | 2026-05-11 06:18:45.345Z | 12.529° NNE | 2026-05-11 06:23:45.345Z | 94.123° ESE | 40.938° | 2026-05-11 06:29:45.345Z | 167.003° S |
| 7 mins | 2026-05-11 08:06:45.345Z | 316.93° NNW | 2026-05-11 08:09:45.345Z | 282.963° WNW | 20.04° | 2026-05-11 08:13:45.345Z | 242.701° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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