QIANFAN-266, 101281
Orbit data source: Space-Track
QIANFAN-266, 101281 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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101281 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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-266
1 A1281U 26248T 26312.31534213 .00000135 00000-0 49238-4 0 9999
2 A1281 88.9892 327.1638 0005588 309.6474 50.4226 14.27418237 757Epoch: 2026-11-08T07:34Z
TLE epoch observation values (Epoch: 2026-11-08T07:34:05.560Z)
Latitude
-0.00006°
Longitude
166.13262°
Altitude
800.882 km
Speed
7.454 km/s
True Right ascension
21h 48m 39s
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
12:11:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
801.324 km
Perigee altitude
793.305 km
Semi-major axis
7,175.451 km
Eccentricity
0.00056
Inclination
88.9892°
RAAN
327.1638°
Arg. of periapsis
309.6474°
True anomaly
50.47198°
Mean anomaly
50.4226°
Eccentric anomaly
50.44729°
Mean motion
3.57083 °/min
Orbital period
100.82 mins
BSTAR
0.000049238
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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-266 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 00:31:35.722Z | 123.729° SE | 2026-11-09 00:35:35.722Z | 69.674° E | 22.458° | 2026-11-09 00:38:35.722Z | 32.126° NE |
| 8 mins | 2026-11-09 02:12:35.722Z | 216.003° SW | 2026-11-09 02:15:35.722Z | 271.849° WNW | 40.56° | 2026-11-09 02:20:35.722Z | 343.747° N |
| 8 mins | 2026-11-09 12:45:35.722Z | 24.184° NE | 2026-11-09 12:49:35.722Z | 90.218° ESE | 37.006° | 2026-11-09 12:53:35.722Z | 148.582° SSE |
| 6 mins | 2026-11-09 14:27:35.722Z | 318.817° NNW | 2026-11-09 14:29:35.722Z | 289.287° WNW | 24.667° | 2026-11-09 14:33:35.722Z | 233.295° 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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