QIANFAN-106, 66048
Orbit data source: Space-Track
QIANFAN-106, 66048 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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66048 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: 16 hours ago
TLE from 16 hours ago
0 QIANFAN-106
1 66048U 25233R 26129.82459425 -.01627449 00000-0 -28938+1 0 9993
2 66048 89.0010 47.0301 0012030 147.1643 213.0255 13.46029535 28018Epoch: 2026-05-09T19:47Z
TLE epoch observation values (Epoch: 2026-05-09T19:47:24.943Z)
Latitude
-0.00002°
Longitude
-117.46031°
Altitude
1,097.383 km
Speed
7.3 km/s
True Right ascension
03h 08m 07s
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
19:44:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,092.938 km
Perigee altitude
1,074.984 km
Semi-major axis
7,462.098 km
Eccentricity
0.0012
Inclination
89.001°
RAAN
47.0301°
Arg. of periapsis
147.1643°
True anomaly
212.95046°
Mean anomaly
213.0255°
Eccentric anomaly
212.98797°
Mean motion
3.36707 °/min
Orbital period
106.92 mins
BSTAR
-2.8938
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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-106 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 17:22:43.954Z | 106.938° ESE | 2026-05-10 17:25:43.954Z | 77.602° E | 17.734° | 2026-05-10 17:29:43.954Z | 37.679° NE |
| 11 mins | 2026-05-10 19:07:43.954Z | 189.876° SSW | 2026-05-10 19:12:43.954Z | 280.881° WNW | 43.258° | 2026-05-10 19:18:43.954Z | 353.808° N |
| 11 mins | 2026-05-11 06:21:43.954Z | 11.549° NNE | 2026-05-11 06:26:43.954Z | 93.463° ESE | 41.711° | 2026-05-11 06:32:43.954Z | 168.265° S |
| 8 mins | 2026-05-11 08:09:43.954Z | 322.932° NNW | 2026-05-11 08:13:43.954Z | 280.779° WNW | 19.535° | 2026-05-11 08:17:43.954Z | 242.706° 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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