QIANFAN-250, 101265
Orbit data source: Space-Track
QIANFAN-250, 101265 is a Chinese payload satellite in LEO that was launched on Tue, 03 Nov 2026 UTC via a LIJIAN-2 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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101265 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 QIANFAN-250
1 A1265U 26248B 26312.03511028 -.00000034 00000-0 -19716-4 0 9997
2 A1265 88.9889 327.1963 0005403 310.3416 49.7305 14.27368212 719Epoch: 2026-11-08T00:50Z
TLE epoch observation values (Epoch: 2026-11-08T00:50:33.528Z)
Latitude
-0.00008°
Longitude
-92.6752°
Altitude
801.099 km
Speed
7.454 km/s
True Right ascension
21h 48m 47s
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
11:59:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
801.359 km
Perigee altitude
793.605 km
Semi-major axis
7,175.619 km
Eccentricity
0.00054
Inclination
88.9889°
RAAN
327.1963°
Arg. of periapsis
310.3416°
True anomaly
49.77776°
Mean anomaly
49.7305°
Eccentric anomaly
49.75413°
Mean motion
3.57071 °/min
Orbital period
100.82 mins
BSTAR
-0.000019716
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Other satellites on launch #248 in the year 2026 (2026-11-03 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-250 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 | 2026-11-09 00:31:41.911Z | 125.464° SE | 2026-11-09 00:35:41.911Z | 72.9° E | 22.789° | 2026-11-09 00:38:41.911Z | 33.697° NE |
| 8 mins | 2026-11-09 02:12:41.911Z | 214.569° SW | 2026-11-09 02:15:41.911Z | 266.129° W | 40.006° | 2026-11-09 02:20:41.911Z | 342.716° N |
| 7 mins | 2026-11-09 12:46:41.911Z | 30.268° NE | 2026-11-09 12:49:41.911Z | 84.437° E | 37.392° | 2026-11-09 12:53:41.911Z | 147.442° SSE |
| 6 mins | 2026-11-09 14:27:41.911Z | 321.166° NNW | 2026-11-09 14:30:41.911Z | 275.538° WNW | 24.597° | 2026-11-09 14:33:41.911Z | 235.364° 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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