QIANFAN-254, 101269
Orbit data source: Space-Track
QIANFAN-254, 101269 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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101269 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-254
1 A1269U 26248F 26312.31545115 .00000135 00000-0 49158-4 0 9999
2 A1269 88.9891 327.1638 0005425 309.2547 50.8166 14.27389091 751Epoch: 2026-11-08T07:34Z
TLE epoch observation values (Epoch: 2026-11-08T07:34:14.979Z)
Latitude
0.00005°
Longitude
166.09327°
Altitude
801.075 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
801.305 km
Perigee altitude
793.519 km
Semi-major axis
7,175.549 km
Eccentricity
0.00054
Inclination
88.9891°
RAAN
327.1638°
Arg. of periapsis
309.2547°
True anomaly
50.86481°
Mean anomaly
50.8166°
Eccentric anomaly
50.8407°
Mean motion
3.57076 °/min
Orbital period
100.82 mins
BSTAR
0.000049158
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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-254 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 00:31:45.695Z | 123.914° SE | 2026-11-09 00:35:45.695Z | 69.842° E | 22.554° | 2026-11-09 00:38:45.695Z | 32.161° NE |
| 8 mins | 2026-11-09 02:12:45.695Z | 216.033° SW | 2026-11-09 02:15:45.695Z | 271.468° WNW | 40.396° | 2026-11-09 02:20:45.695Z | 343.617° N |
| 8 mins | 2026-11-09 12:45:45.695Z | 23.913° NE | 2026-11-09 12:49:45.695Z | 89.568° E | 37.19° | 2026-11-09 12:53:45.695Z | 148.562° SSE |
| 6 mins | 2026-11-09 14:27:45.695Z | 319.059° NNW | 2026-11-09 14:29:45.695Z | 289.752° WNW | 24.535° | 2026-11-09 14:33:45.695Z | 233.629° 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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