QIANFAN-150, 69109
Orbit data source: Space-Track
QIANFAN-150, 69109 is a Chinese payload satellite in LEO that was launched on Sun, 17 May 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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69109 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 shape, 14.5 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 QIANFAN-150
1 69109U 26108F 26170.97179105 -.00000041 00000-0 -35639-4 0 9994
2 69109 89.0123 21.9198 0018588 99.3077 261.0206 14.02932758 4737Epoch: 2026-06-19T23:19Z
TLE epoch observation values (Epoch: 2026-06-19T23:19:22.746Z)
Latitude
-0.00009°
Longitude
123.88192°
Altitude
888.818 km
Speed
7.407 km/s
True Right ascension
01h 27m 40s
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
07:15:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
894.125 km
Perigee altitude
867.14 km
Semi-major axis
7,258.77 km
Eccentricity
0.00186
Inclination
89.0123°
RAAN
21.9198°
Arg. of periapsis
99.3077°
True anomaly
260.81028°
Mean anomaly
261.0206°
Eccentric anomaly
260.91543°
Mean motion
3.50953 °/min
Orbital period
102.58 mins
BSTAR
-0.000035639
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Other satellites on launch #108 in the year 2026 (2026-05-17 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-150 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 01:35:27.755Z | 24.251° NE | 2026-06-21 01:39:27.755Z | 78.672° E | 29.349° | 2026-06-21 01:44:27.755Z | 146.929° SSE |
| 8 mins | 2026-06-21 03:18:27.755Z | 332.022° NNW | 2026-06-21 03:22:27.755Z | 275.311° WNW | 26.079° | 2026-06-21 03:26:27.755Z | 225.487° WSW |
| 6 mins | 2026-06-21 13:08:27.755Z | 104.472° ESE | 2026-06-21 13:10:27.755Z | 80.846° E | 16.754° | 2026-06-21 13:14:27.755Z | 35.416° NE |
| 10 mins | 2026-06-21 14:48:27.755Z | 195.226° SSW | 2026-06-21 14:53:27.755Z | 294.484° NW | 39.82° | 2026-06-21 14:58:27.755Z | 350.964° 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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