QIANFAN-193, 69411
Orbit data source: Space-Track
QIANFAN-193, 69411 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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69411 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: 15 hours ago
TLE from 15 hours ago
0 QIANFAN-193
1 69411U 26125L 26171.20259476 -.01725353 00000-0 -94876+0 0 9990
2 69411 88.9948 280.1006 0016730 173.7424 186.3976 14.15759213 2135Epoch: 2026-06-20T04:51Z
TLE epoch observation values (Epoch: 2026-06-20T04:51:44.187Z)
Latitude
0°
Longitude
-61.25411°
Altitude
854.781 km
Speed
7.419 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
07:15:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
848.758 km
Perigee altitude
824.618 km
Semi-major axis
7,214.825 km
Eccentricity
0.00167
Inclination
88.9948°
RAAN
280.1006°
Arg. of periapsis
173.7424°
True anomaly
186.37628°
Mean anomaly
186.3976°
Eccentric anomaly
186.38694°
Mean motion
3.54164 °/min
Orbital period
101.65 mins
BSTAR
-0.94876
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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-193 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 | 2026-06-20 20:44:17.334Z | 326.304° NNW | 2026-06-20 20:47:17.334Z | 288.959° WNW | 20.78° | 2026-06-20 20:51:17.334Z | 237.198° WSW |
| 5 mins | 2026-06-21 06:30:17.334Z | 103.646° ESE | 2026-06-21 06:32:17.334Z | 76.868° E | 19.005° | 2026-06-21 06:35:17.334Z | 39.274° NE |
| 8 mins | 2026-06-21 08:10:17.334Z | 205.225° SW | 2026-06-21 08:14:17.334Z | 288.056° WNW | 37.194° | 2026-06-21 08:18:17.334Z | 344.683° N |
| 8 mins | 2026-06-21 18:51:17.334Z | 25.896° NE | 2026-06-21 18:55:17.334Z | 93.714° ESE | 31.206° | 2026-06-21 18:59:17.334Z | 148.625° 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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