QIANFAN-160, 69119
Orbit data source: Space-Track
QIANFAN-160, 69119 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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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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-160
1 69119U 26108R 26171.47410890 -.00000045 00000-0 -37597-4 0 9999
2 69119 89.0109 21.8400 0016851 97.5292 262.7804 14.03743498 4810Epoch: 2026-06-20T11:22Z
TLE epoch observation values (Epoch: 2026-06-20T11:22:43.008Z)
Latitude
-0.00005°
Longitude
-57.52742°
Altitude
885.449 km
Speed
7.409 km/s
True Right ascension
01h 27m 21s
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
07:13:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
890.062 km
Perigee altitude
865.608 km
Semi-major axis
7,255.972 km
Eccentricity
0.00169
Inclination
89.0109°
RAAN
21.84°
Arg. of periapsis
97.5292°
True anomaly
262.58888°
Mean anomaly
262.7804°
Eccentric anomaly
262.68464°
Mean motion
3.51156 °/min
Orbital period
102.52 mins
BSTAR
-0.000037597
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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-160 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 01:38:54.032Z | 19.956° NNE | 2026-06-21 01:43:54.032Z | 91.204° ESE | 31.039° | 2026-06-21 01:47:54.032Z | 146.909° SSE |
| 7 mins | 2026-06-21 03:22:54.032Z | 325.437° NNW | 2026-06-21 03:25:54.032Z | 282.868° WNW | 24.561° | 2026-06-21 03:29:54.032Z | 230.445° WSW |
| 6 mins | 2026-06-21 13:11:54.032Z | 106.26° ESE | 2026-06-21 13:13:54.032Z | 81.846° E | 17.854° | 2026-06-21 13:17:54.032Z | 34.883° NE |
| 10 mins | 2026-06-21 14:51:54.032Z | 198.001° SSW | 2026-06-21 14:56:54.032Z | 291.82° WNW | 38.5° | 2026-06-21 15:01:54.032Z | 349.666° 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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