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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-106
1 66048U 25233R 26177.59680872 .00000090 00000-0 12130-3 0 9996
2 66048 88.9988 42.2038 0002310 87.4687 272.6729 13.51013304 34453Epoch: 2026-06-26T14:19Z
TLE epoch observation values (Epoch: 2026-06-26T14:19:24.273Z)
Latitude
0.00002°
Longitude
-87.37038°
Altitude
1,071.406 km
Speed
7.316 km/s
True Right ascension
02h 48m 48s
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
12:09:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,067.303 km
Perigee altitude
1,063.864 km
Semi-major axis
7,443.721 km
Eccentricity
0.00023
Inclination
88.9988°
RAAN
42.2038°
Arg. of periapsis
87.4687°
True anomaly
272.64646°
Mean anomaly
272.6729°
Eccentric anomaly
272.65968°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.0001213
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-27 01:37:25.341Z | 49.693° ENE | 2026-06-27 01:40:25.341Z | 78.271° E | 13.554° | 2026-06-27 01:42:25.341Z | 97.183° ESE |
| 11 mins | 2026-06-27 03:22:25.341Z | 359.77° N | 2026-06-27 03:27:25.341Z | 263.453° W | 44.941° | 2026-06-27 03:33:25.341Z | 184.634° SSW |
| 4 mins | 2026-06-27 05:11:25.341Z | 303.808° NW | 2026-06-27 05:12:25.341Z | 294.439° NW | 12.388° | 2026-06-27 05:15:25.341Z | 266.859° W |
| 11 mins | 2026-06-27 15:19:25.341Z | 173.403° S | 2026-06-27 15:24:25.341Z | 64.903° ENE | 44.783° | 2026-06-27 15:30:25.341Z | 0.872° NNE |
| 5 mins | 2026-06-27 17:09:25.341Z | 263.618° W | 2026-06-27 17:11:25.341Z | 283.082° WNW | 14.182° | 2026-06-27 17:14:25.341Z | 311.88° NW |
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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