QIANFAN-161, 69120
Orbit data source: Space-Track
QIANFAN-161, 69120 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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69120 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-161
1 69120U 26108S 26171.38036811 .00000120 00000-0 63840-4 0 9990
2 69120 89.0112 21.8449 0016748 101.4715 258.8350 14.06834942 4808Epoch: 2026-06-20T09:07Z
TLE epoch observation values (Epoch: 2026-06-20T09:07:43.804Z)
Latitude
0.00001°
Longitude
-23.68344°
Altitude
875.628 km
Speed
7.413 km/s
True Right ascension
01h 27m 22s
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
07:17:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
879.327 km
Perigee altitude
855.058 km
Semi-major axis
7,245.33 km
Eccentricity
0.00167
Inclination
89.0112°
RAAN
21.8449°
Arg. of periapsis
101.4715°
True anomaly
258.64679°
Mean anomaly
258.835°
Eccentric anomaly
258.74089°
Mean motion
3.5193 °/min
Orbital period
102.29 mins
BSTAR
0.00006384
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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-161 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 01:05:48.621Z | 41.858° NE | 2026-06-21 01:08:48.621Z | 77.621° E | 17.527° | 2026-06-21 01:11:48.621Z | 114.22° SE |
| 9 mins | 2026-06-21 02:47:48.621Z | 345.974° N | 2026-06-21 02:51:48.621Z | 266.328° W | 39.006° | 2026-06-21 02:56:48.621Z | 200.407° SSW |
| 9 mins | 2026-06-21 14:15:48.621Z | 168.102° S | 2026-06-21 14:19:48.621Z | 121.846° SE | 42.979° | 2026-06-21 14:24:48.621Z | 4.583° NNE |
| 4 mins | 2026-06-21 16:01:48.621Z | 267.97° W | 2026-06-21 16:02:48.621Z | 279.415° WNW | 13.363° | 2026-06-21 16:05:48.621Z | 312.389° NW |
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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