QIANFAN-255, 101270
Orbit data source: Space-Track
QIANFAN-255, 101270 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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101270 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: 17 hours ago
TLE from 17 hours ago
0 QIANFAN-255
1 A1270U 26248G 26311.96484071 .00000129 00000-0 46563-4 0 9994
2 A1270 88.9891 327.2044 0005577 311.6183 48.4533 14.27416677 703Epoch: 2026-11-07T23:09Z
TLE epoch observation values (Epoch: 2026-11-07T23:09:22.237Z)
Latitude
-0.00001°
Longitude
-67.30079°
Altitude
800.788 km
Speed
7.454 km/s
True Right ascension
21h 48m 49s
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
11:59:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
801.321 km
Perigee altitude
793.318 km
Semi-major axis
7,175.457 km
Eccentricity
0.00056
Inclination
88.9891°
RAAN
327.2044°
Arg. of periapsis
311.6183°
True anomaly
48.50115°
Mean anomaly
48.4533°
Eccentric anomaly
48.47722°
Mean motion
3.57083 °/min
Orbital period
100.82 mins
BSTAR
0.000046563
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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-255 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 00:31:46.174Z | 122.336° SE | 2026-11-09 00:34:46.174Z | 83.577° E | 22.587° | 2026-11-09 00:38:46.174Z | 30.788° NE |
| 8 mins | 2026-11-09 02:11:46.174Z | 209.853° SW | 2026-11-09 02:15:46.174Z | 276.659° WNW | 40.55° | 2026-11-09 02:19:46.174Z | 339.515° N |
| 8 mins | 2026-11-09 12:45:46.174Z | 25.351° NE | 2026-11-09 12:49:46.174Z | 94.452° ESE | 36.717° | 2026-11-09 12:53:46.174Z | 149.54° SSE |
| 7 mins | 2026-11-09 14:26:46.174Z | 327.201° NNW | 2026-11-09 14:29:46.174Z | 286.382° WNW | 24.831° | 2026-11-09 14:33:46.174Z | 232.001° 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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