QIANFAN-175, 69392
Orbit data source: Space-Track
QIANFAN-175, 69392 is a Chinese payload satellite in LEO that was launched on Thu, 04 Jun 2026 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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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69392 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH
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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-175
1 69392U 26124L 26171.47456774 .00000089 00000-0 33953-4 0 9999
2 69392 88.9983 1.6597 0003669 160.1847 199.9487 14.21339841 2280Epoch: 2026-06-20T11:23Z
TLE epoch observation values (Epoch: 2026-06-20T11:23:22.652Z)
Latitude
-0.00004°
Longitude
-77.87335°
Altitude
826.364 km
Speed
7.438 km/s
True Right ascension
00h 06m 38s
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
07:14:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
820.415 km
Perigee altitude
815.134 km
Semi-major axis
7,195.911 km
Eccentricity
0.00037
Inclination
88.9983°
RAAN
1.6597°
Arg. of periapsis
160.1847°
True anomaly
199.93436°
Mean anomaly
199.9487°
Eccentric anomaly
199.94153°
Mean motion
3.55561 °/min
Orbital period
101.25 mins
BSTAR
0.000033953
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Other satellites on launch #124 in the year 2026 (2026-06-04 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-175 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 23:49:22.361Z | 44.292° NE | 2026-06-20 23:52:22.361Z | 83.172° E | 17.807° | 2026-06-20 23:55:22.361Z | 119.608° SE |
| 8 mins | 2026-06-21 01:30:22.361Z | 342.162° N | 2026-06-21 01:33:22.361Z | 288.925° WNW | 37.231° | 2026-06-21 01:38:22.361Z | 203.816° SW |
| 9 mins | 2026-06-21 12:51:22.361Z | 163.161° S | 2026-06-21 12:55:22.361Z | 80.716° E | 42.163° | 2026-06-21 13:00:22.361Z | 5.778° NNE |
| 4 mins | 2026-06-21 14:35:22.361Z | 261.88° W | 2026-06-21 14:37:22.361Z | 286.269° WNW | 14.157° | 2026-06-21 14:39:22.361Z | 309.554° NW |
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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