QIANFAN-265, 101280
Orbit data source: Space-Track
QIANFAN-265, 101280 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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101280 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-265
1 A1280U 26248S 26312.31521324 .00000135 00000-0 48989-4 0 9999
2 A1280 88.9891 327.1637 0005647 310.8953 49.1752 14.27453190 752Epoch: 2026-11-08T07:33Z
TLE epoch observation values (Epoch: 2026-11-08T07:33:54.423Z)
Latitude
-0.00001°
Longitude
166.17906°
Altitude
800.671 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
11:59:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
801.249 km
Perigee altitude
793.145 km
Semi-major axis
7,175.334 km
Eccentricity
0.00056
Inclination
88.9891°
RAAN
327.1637°
Arg. of periapsis
310.8953°
True anomaly
49.22419°
Mean anomaly
49.1752°
Eccentric anomaly
49.19969°
Mean motion
3.57092 °/min
Orbital period
100.81 mins
BSTAR
0.000048989
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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-265 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 00:31:40.900Z | 121.061° SE | 2026-11-09 00:34:40.900Z | 81.373° E | 22.578° | 2026-11-09 00:38:40.900Z | 29.839° NE |
| 8 mins | 2026-11-09 02:11:40.900Z | 210.536° SW | 2026-11-09 02:15:40.900Z | 280.592° WNW | 40.573° | 2026-11-09 02:19:40.900Z | 340.385° N |
| 8 mins | 2026-11-09 12:45:40.900Z | 26.61° NE | 2026-11-09 12:48:40.900Z | 72.611° E | 36.204° | 2026-11-09 12:53:40.900Z | 150.203° SSE |
| 7 mins | 2026-11-09 14:26:40.900Z | 325.914° NNW | 2026-11-09 14:29:40.900Z | 283.667° WNW | 25.038° | 2026-11-09 14:33:40.900Z | 230.717° 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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