QIANFAN-158, 69117
Orbit data source: Space-Track
QIANFAN-158, 69117 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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69117 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: 11 hours ago
TLE from 11 hours ago
0 QIANFAN-158
1 69117U 26108P 26171.40522785 -.00000035 00000-0 -29728-4 0 9993
2 69117 89.0107 21.8476 0017358 99.2170 261.0976 14.06065312 4802Epoch: 2026-06-20T09:43Z
TLE epoch observation values (Epoch: 2026-06-20T09:43:31.686Z)
Latitude
-0.00006°
Longitude
-32.65475°
Altitude
877.87 km
Speed
7.412 km/s
True Right ascension
01h 27m 23s
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
07:15:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
882.42 km
Perigee altitude
857.258 km
Semi-major axis
7,247.976 km
Eccentricity
0.00174
Inclination
89.0107°
RAAN
21.8476°
Arg. of periapsis
99.217°
True anomaly
260.90115°
Mean anomaly
261.0976°
Eccentric anomaly
260.99937°
Mean motion
3.51737 °/min
Orbital period
102.35 mins
BSTAR
-0.000029728
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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-158 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 01:40:24.539Z | 17.468° NNE | 2026-06-21 01:45:24.539Z | 82.487° E | 31.809° | 2026-06-21 01:50:24.539Z | 151.652° SSE |
| 7 mins | 2026-06-21 03:24:24.539Z | 326.543° NNW | 2026-06-21 03:27:24.539Z | 286.092° WNW | 23.661° | 2026-06-21 03:31:24.539Z | 232.716° WSW |
| 6 mins | 2026-06-21 13:12:24.539Z | 108.795° ESE | 2026-06-21 13:15:24.539Z | 71.069° E | 17.995° | 2026-06-21 13:18:24.539Z | 36.462° NE |
| 9 mins | 2026-06-21 14:53:24.539Z | 202.837° SW | 2026-06-21 14:57:24.539Z | 289.534° WNW | 38.319° | 2026-06-21 15:02:24.539Z | 349.34° 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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