QIANFAN-149, 69108
Orbit data source: Space-Track
QIANFAN-149, 69108 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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69108 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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-149
1 69108U 26108E 26171.28483503 .00000050 00000-0 25889-4 0 9992
2 69108 89.0106 21.8847 0017370 99.2134 261.1010 13.97773674 4779Epoch: 2026-06-20T06:50Z
TLE epoch observation values (Epoch: 2026-06-20T06:50:09.746Z)
Latitude
0.00005°
Longitude
10.84243°
Altitude
906.514 km
Speed
7.398 km/s
True Right ascension
01h 27m 32s
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
07:14:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
911.137 km
Perigee altitude
885.858 km
Semi-major axis
7,276.635 km
Eccentricity
0.00174
Inclination
89.0106°
RAAN
21.8847°
Arg. of periapsis
99.2134°
True anomaly
260.90442°
Mean anomaly
261.101°
Eccentric anomaly
261.0027°
Mean motion
3.49661 °/min
Orbital period
102.96 mins
BSTAR
0.000025889
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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-149 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 02:19:14.761Z | 2.421° NNE | 2026-06-21 02:24:14.761Z | 135.454° SSE | 44.809° | 2026-06-21 02:29:14.761Z | 180.301° SSW |
| 9 mins | 2026-06-21 13:53:14.761Z | 147.318° SSE | 2026-06-21 13:57:14.761Z | 82.277° E | 35.434° | 2026-06-21 14:02:14.761Z | 13.397° NNE |
| 7 mins | 2026-06-21 15:37:14.761Z | 238.418° WSW | 2026-06-21 15:40:14.761Z | 276.741° WNW | 21.357° | 2026-06-21 15:44:14.761Z | 326.065° NNW |
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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