QIANFAN-159, 69118
Orbit data source: Space-Track
QIANFAN-159, 69118 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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69118 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-159
1 69118U 26108Q 26170.97512209 -.00000046 00000-0 -37403-4 0 9996
2 69118 89.0101 21.8932 0017478 96.8618 263.4553 14.04703438 4743Epoch: 2026-06-19T23:24Z
TLE epoch observation values (Epoch: 2026-06-19T23:24:10.548Z)
Latitude
0.00001°
Longitude
122.65286°
Altitude
882.052 km
Speed
7.41 km/s
True Right ascension
01h 27m 34s
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
07:16:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
887.203 km
Perigee altitude
861.85 km
Semi-major axis
7,252.664 km
Eccentricity
0.00175
Inclination
89.0101°
RAAN
21.8932°
Arg. of periapsis
96.8618°
True anomaly
263.25637°
Mean anomaly
263.4553°
Eccentric anomaly
263.35583°
Mean motion
3.51396 °/min
Orbital period
102.45 mins
BSTAR
-0.000037403
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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-159 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 01:37:49.633Z | 20.465° NNE | 2026-06-21 01:42:49.633Z | 91.517° ESE | 30.483° | 2026-06-21 01:46:49.633Z | 146.314° SSE |
| 7 mins | 2026-06-21 03:21:49.633Z | 325.06° NNW | 2026-06-21 03:24:49.633Z | 281.258° WNW | 24.956° | 2026-06-21 03:28:49.633Z | 229.137° WSW |
| 5 mins | 2026-06-21 13:10:49.633Z | 100.534° ESE | 2026-06-21 13:12:49.633Z | 75.144° E | 17.414° | 2026-06-21 13:15:49.633Z | 39.69° NE |
| 9 mins | 2026-06-21 14:50:49.633Z | 198.953° SSW | 2026-06-21 14:54:49.633Z | 274.148° WNW | 39.724° | 2026-06-21 14:59:49.633Z | 349.047° 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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