QIANFAN-199, 69417
Orbit data source: Space-Track
QIANFAN-199, 69417 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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69417 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-199
1 69417U 26125S 26170.77152315 -.01926055 00000-0 -97995+0 0 9998
2 69417 88.9945 280.1474 0014695 175.6046 184.5276 14.19732489 2072Epoch: 2026-06-19T18:30Z
TLE epoch observation values (Epoch: 2026-06-19T18:30:59.600Z)
Latitude
0.00002°
Longitude
94.40335°
Altitude
839.866 km
Speed
7.427 km/s
True Right ascension
18h 40m 35s
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
07:12:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
833.792 km
Perigee altitude
812.627 km
Semi-major axis
7,201.346 km
Eccentricity
0.00147
Inclination
88.9945°
RAAN
280.1474°
Arg. of periapsis
175.6046°
True anomaly
184.51433°
Mean anomaly
184.5276°
Eccentric anomaly
184.52096°
Mean motion
3.55159 °/min
Orbital period
101.36 mins
BSTAR
-0.97995
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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-199 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 | 2026-06-20 20:30:24.562Z | 338.055° N | 2026-06-20 20:35:24.562Z | 271.565° WNW | 25.523° | 2026-06-20 20:39:24.562Z | 223.363° SW |
| 4 mins | 2026-06-21 06:17:24.562Z | 90.854° ESE | 2026-06-21 06:18:24.562Z | 78.979° E | 14.387° | 2026-06-21 06:21:24.562Z | 44.63° NE |
| 9 mins | 2026-06-21 07:56:24.562Z | 192.127° SSW | 2026-06-21 08:00:24.562Z | 298.122° NW | 42.179° | 2026-06-21 08:05:24.562Z | 353.517° N |
| 7 mins | 2026-06-21 18:37:24.562Z | 40.111° NE | 2026-06-21 18:40:24.562Z | 87.477° E | 24.911° | 2026-06-21 18:44:24.562Z | 138.121° SSE |
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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