QIANFAN-168, 69385
Orbit data source: Space-Track
QIANFAN-168, 69385 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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69385 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-168
1 69385U 26124D 26171.42462499 .00000076 00000-0 30067-4 0 9996
2 69385 88.9983 1.6709 0003344 126.7659 233.3838 14.17873249 2278Epoch: 2026-06-20T10:11Z
TLE epoch observation values (Epoch: 2026-06-20T10:11:27.599Z)
Latitude
0.00007°
Longitude
-59.83354°
Altitude
837.043 km
Speed
7.434 km/s
True Right ascension
00h 06m 41s
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
07:12:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
831.919 km
Perigee altitude
827.098 km
Semi-major axis
7,207.646 km
Eccentricity
0.00033
Inclination
88.9983°
RAAN
1.6709°
Arg. of periapsis
126.7659°
True anomaly
233.35305°
Mean anomaly
233.3838°
Eccentric anomaly
233.36842°
Mean motion
3.54693 °/min
Orbital period
101.5 mins
BSTAR
0.000030067
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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-168 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 00:19:12.706Z | 19.759° NNE | 2026-06-21 00:24:12.706Z | 92.877° ESE | 30.537° | 2026-06-21 00:28:12.706Z | 147.965° SSE |
| 7 mins | 2026-06-21 02:02:12.706Z | 325.001° NNW | 2026-06-21 02:05:12.706Z | 281.45° WNW | 23.788° | 2026-06-21 02:09:12.706Z | 229.463° WSW |
| 4 mins | 2026-06-21 11:46:12.706Z | 93.683° ESE | 2026-06-21 11:48:12.706Z | 68.587° E | 15.012° | 2026-06-21 11:50:12.706Z | 45.407° ENE |
| 8 mins | 2026-06-21 13:25:12.706Z | 195.752° SSW | 2026-06-21 13:28:12.706Z | 244.427° WSW | 40.795° | 2026-06-21 13:33:12.706Z | 350.127° 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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