QIANFAN-264, 101279
Orbit data source: Space-Track
QIANFAN-264, 101279 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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101279 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-264
1 A1279U 26248R 26312.31524151 .00000135 00000-0 49250-4 0 9990
2 A1279 88.9892 327.1637 0005627 310.7946 49.2760 14.27445565 757Epoch: 2026-11-08T07:33Z
TLE epoch observation values (Epoch: 2026-11-08T07:33:56.866Z)
Latitude
0.00002°
Longitude
166.16885°
Altitude
800.711 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
11:59:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
801.26 km
Perigee altitude
793.185 km
Semi-major axis
7,175.36 km
Eccentricity
0.00056
Inclination
88.9892°
RAAN
327.1637°
Arg. of periapsis
310.7946°
True anomaly
49.32489°
Mean anomaly
49.276°
Eccentric anomaly
49.30044°
Mean motion
3.5709 °/min
Orbital period
100.81 mins
BSTAR
0.00004925
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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-264 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 00:31:45.210Z | 120.852° SE | 2026-11-09 00:34:45.210Z | 80.947° E | 22.615° | 2026-11-09 00:38:45.210Z | 29.629° NE |
| 8 mins | 2026-11-09 02:11:45.210Z | 210.736° SW | 2026-11-09 02:15:45.210Z | 281.312° WNW | 40.486° | 2026-11-09 02:19:45.210Z | 340.502° N |
| 8 mins | 2026-11-09 12:45:45.210Z | 26.756° NE | 2026-11-09 12:48:45.210Z | 73.14° E | 36.305° | 2026-11-09 12:53:45.210Z | 150.352° SSE |
| 7 mins | 2026-11-09 14:26:45.210Z | 325.698° NNW | 2026-11-09 14:29:45.210Z | 283.283° WNW | 25.019° | 2026-11-09 14:33:45.210Z | 230.588° 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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