QIANFAN-151, 69110
Orbit data source: Space-Track
QIANFAN-151, 69110 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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69110 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-151
1 69110U 26108G 26170.97327586 -.00000020 00000-0 -22952-4 0 9995
2 69110 89.0109 21.9125 0017989 98.4586 261.8634 14.00814396 4730Epoch: 2026-06-19T23:21Z
TLE epoch observation values (Epoch: 2026-06-19T23:21:31.034Z)
Latitude
0.00007°
Longitude
123.33862°
Altitude
895.876 km
Speed
7.403 km/s
True Right ascension
01h 27m 39s
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
07:12:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
901.026 km
Perigee altitude
874.884 km
Semi-major axis
7,266.092 km
Eccentricity
0.0018
Inclination
89.0109°
RAAN
21.9125°
Arg. of periapsis
98.4586°
True anomaly
261.6594°
Mean anomaly
261.8634°
Eccentric anomaly
261.76139°
Mean motion
3.50422 °/min
Orbital period
102.73 mins
BSTAR
-0.000022952
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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-151 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-21 01:39:28.965Z | 19.586° NNE | 2026-06-21 01:44:28.965Z | 90.301° ESE | 31.483° | 2026-06-21 01:49:28.965Z | 152.187° SSE |
| 7 mins | 2026-06-21 03:23:28.965Z | 327.373° NNW | 2026-06-21 03:26:28.965Z | 287.307° WNW | 24.347° | 2026-06-21 03:30:28.965Z | 232.838° WSW |
| 6 mins | 2026-06-21 13:13:28.965Z | 111.758° ESE | 2026-06-21 13:16:28.965Z | 74.763° E | 18.86° | 2026-06-21 13:19:28.965Z | 38.538° NE |
| 9 mins | 2026-06-21 14:54:28.965Z | 201.003° SSW | 2026-06-21 14:58:28.965Z | 264.079° W | 38.201° | 2026-06-21 15:03:28.965Z | 346.489° 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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