QIANFAN-191, 69409
Orbit data source: Space-Track
QIANFAN-191, 69409 is a Chinese payload satellite in LEO that was launched on Fri, 05 Jun 2026 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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69409 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
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 QIANFAN-191
1 69409U 26125J 26170.71553640 -.01819046 00000-0 -99942+0 0 9994
2 69409 88.9947 280.1576 0012443 170.0084 190.1353 14.15407399 2061Epoch: 2026-06-19T17:10Z
TLE epoch observation values (Epoch: 2026-06-19T17:10:22.344Z)
Latitude
-0.00008°
Longitude
114.62397°
Altitude
852.818 km
Speed
7.422 km/s
True Right ascension
18h 40m 37s
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
07:12:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
846.863 km
Perigee altitude
828.906 km
Semi-major axis
7,216.021 km
Eccentricity
0.00124
Inclination
88.9947°
RAAN
280.1576°
Arg. of periapsis
170.0084°
True anomaly
190.11025°
Mean anomaly
190.1353°
Eccentric anomaly
190.12277°
Mean motion
3.54076 °/min
Orbital period
101.67 mins
BSTAR
-0.99942
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Other satellites on launch #125 in the year 2026 (2026-06-05 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-191 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 20:58:17.230Z | 315.074° NNW | 2026-06-20 21:00:17.230Z | 291.198° WNW | 16.47° | 2026-06-20 21:03:17.230Z | 254.094° W |
| 7 mins | 2026-06-21 06:43:17.230Z | 122.401° SE | 2026-06-21 06:46:17.230Z | 79.884° E | 24.296° | 2026-06-21 06:50:17.230Z | 27.726° NE |
| 9 mins | 2026-06-21 08:24:17.230Z | 214.249° SW | 2026-06-21 08:28:17.230Z | 275.169° WNW | 31.372° | 2026-06-21 08:33:17.230Z | 341.667° N |
| 9 mins | 2026-06-21 19:06:17.230Z | 15.743° NNE | 2026-06-21 19:10:17.230Z | 82.846° E | 38.365° | 2026-06-21 19:15:17.230Z | 162.313° S |
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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