QIANFAN-165, 69382
Orbit data source: Space-Track
QIANFAN-165, 69382 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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69382 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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-165
1 69382U 26124A 26171.36621924 .00000056 00000-0 21393-4 0 9996
2 69382 88.9984 1.6807 0003165 115.0946 245.0571 14.16012697 2260Epoch: 2026-06-20T08:47Z
TLE epoch observation values (Epoch: 2026-06-20T08:47:21.342Z)
Latitude
0.00003°
Longitude
-38.7401°
Altitude
842.881 km
Speed
7.431 km/s
True Right ascension
00h 06m 43s
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
07:13:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
838.109 km
Perigee altitude
833.543 km
Semi-major axis
7,213.963 km
Eccentricity
0.00032
Inclination
88.9984°
RAAN
1.6807°
Arg. of periapsis
115.0946°
True anomaly
245.02422°
Mean anomaly
245.0571°
Eccentric anomaly
245.04066°
Mean motion
3.54228 °/min
Orbital period
101.63 mins
BSTAR
0.000021393
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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-165 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 | 2026-06-21 00:38:09.142Z | 12.589° NNE | 2026-06-21 00:43:09.142Z | 106.287° ESE | 38.707° | 2026-06-21 00:47:09.142Z | 162.688° S |
| 5 mins | 2026-06-21 02:22:09.142Z | 307.322° NW | 2026-06-21 02:24:09.142Z | 280.879° WNW | 17.084° | 2026-06-21 02:27:09.142Z | 246.049° WSW |
| 7 mins | 2026-06-21 12:04:09.142Z | 119.176° SE | 2026-06-21 12:07:09.142Z | 78.003° E | 21.951° | 2026-06-21 12:11:09.142Z | 28.376° NE |
| 8 mins | 2026-06-21 13:45:09.142Z | 214.407° SW | 2026-06-21 13:48:09.142Z | 263.321° W | 32.865° | 2026-06-21 13:53:09.142Z | 341.744° N |
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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