QIANFAN-192, 69410
Orbit data source: Space-Track
QIANFAN-192, 69410 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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69410 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: 17 hours ago
TLE from 17 hours ago
0 QIANFAN-192
1 69410U 26125K 26171.20592247 -.01722977 00000-0 -94715+0 0 9996
2 69410 88.9949 280.1013 0012663 156.7497 203.4267 14.15802162 2131Epoch: 2026-06-20T04:56Z
TLE epoch observation values (Epoch: 2026-06-20T04:56:31.701Z)
Latitude
0.00007°
Longitude
-62.45466°
Altitude
851.022 km
Speed
7.423 km/s
True Right ascension
18h 40m 24s
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
08:33:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
845.678 km
Perigee altitude
827.406 km
Semi-major axis
7,214.679 km
Eccentricity
0.00127
Inclination
88.9949°
RAAN
280.1013°
Arg. of periapsis
156.7497°
True anomaly
203.36909°
Mean anomaly
203.4267°
Eccentric anomaly
203.39789°
Mean motion
3.54175 °/min
Orbital period
101.64 mins
BSTAR
-0.94715
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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-192 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 | 2026-06-21 06:33:27.737Z | 120.914° SE | 2026-06-21 06:37:27.737Z | 69.892° E | 20.367° | 2026-06-21 06:40:27.737Z | 33.75° NE |
| 9 mins | 2026-06-21 08:14:27.737Z | 205.945° SW | 2026-06-21 08:18:27.737Z | 268.943° W | 35.47° | 2026-06-21 08:23:27.737Z | 344.571° N |
| 9 mins | 2026-06-21 18:55:27.737Z | 20.349° NNE | 2026-06-21 18:59:27.737Z | 80.413° E | 33.487° | 2026-06-21 19:04:27.737Z | 154.33° SSE |
| 7 mins | 2026-06-21 20:38:27.737Z | 323.007° NNW | 2026-06-21 20:41:27.737Z | 282.097° WNW | 21.894° | 2026-06-21 20:45:27.737Z | 233.069° 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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