QIANFAN-248, 100701
Orbit data source: Space-Track
QIANFAN-248, 100701 is a Chinese payload satellite in LEO that was launched on Tue, 15 Sep 2026 UTC launched 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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100701 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM
Mission
Operational spacecraft
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
BOX+PAN, 5.0 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 QIANFAN-248
1 A0701U 26210K 26261.39371370 .00000048 00000-0 24403-4 0 9998
2 A0701 89.0059 12.5935 0007343 288.6462 71.3918 13.97510232 449Epoch: 2026-09-18T09:26Z
TLE epoch observation values (Epoch: 2026-09-18T09:26:56.863Z)
Latitude
-0.00002°
Longitude
-126.46067°
Altitude
903.748 km
Speed
7.401 km/s
True Right ascension
00h 50m 22s
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
03:40:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
904.757 km
Perigee altitude
894.069 km
Semi-major axis
7,277.55 km
Eccentricity
0.00073
Inclination
89.0059°
RAAN
12.5935°
Arg. of periapsis
288.6462°
True anomaly
71.47157°
Mean anomaly
71.3918°
Eccentric anomaly
71.43168°
Mean motion
3.49595 °/min
Orbital period
102.98 mins
BSTAR
0.000024403
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Other satellites on launch #210 in the year 2026 (2026-09-15 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-248 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-19 18:41:14.668Z | 27.811° NE | 2026-09-19 18:46:14.668Z | 87.31° E | 24.557° | 2026-09-19 18:50:14.668Z | 132.836° SE |
| 9 mins | 2026-09-19 20:25:14.668Z | 339.296° N | 2026-09-19 20:29:14.668Z | 271.272° WNW | 43.188° | 2026-09-19 20:34:14.668Z | 209.093° SW |
| 9 mins | 2026-09-20 07:58:14.668Z | 183.046° SSW | 2026-09-20 08:02:14.668Z | 287.302° WNW | 80.757° | 2026-09-20 08:07:14.668Z | 356.534° N |
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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