QIANFAN-164, 69326
Orbit data source: Space-Track
QIANFAN-164, 69326 is a Chinese payload satellite in LEO that was launched on Mon, 01 Jun 2026 UTC via a CHANG ZHENG 12B launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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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69326 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH
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
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-164
1 69326U 26121B 26153.29254426 -.00000157 00000-0 -22446-3 0 9995
2 69326 89.0156 302.0220 0018101 233.6369 126.3117 13.60503212 137Epoch: 2026-06-02T07:01Z
TLE epoch observation values (Epoch: 2026-06-02T07:01:15.824Z)
Latitude
-0.00008°
Longitude
-54.06154°
Altitude
1,044.793 km
Speed
7.325 km/s
True Right ascension
20h 08m 05s
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
03:08:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,044.312 km
Perigee altitude
1,017.49 km
Semi-major axis
7,409.038 km
Eccentricity
0.00181
Inclination
89.0156°
RAAN
302.022°
Arg. of periapsis
233.6369°
True anomaly
126.47862°
Mean anomaly
126.3117°
Eccentric anomaly
126.39518°
Mean motion
3.4033 °/min
Orbital period
105.78 mins
BSTAR
-0.00022446
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Other satellites on launch #121 in the year 2026 (2026-06-01 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-164 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-06-02 21:43:34.134Z | 10.517° NNE | 2026-06-02 21:49:34.134Z | 79.675° E | 38.744° | 2026-06-02 21:55:34.134Z | 162.405° S |
| 8 mins | 2026-06-02 23:31:34.134Z | 324.446° NNW | 2026-06-02 23:35:34.134Z | 278.039° WNW | 21.424° | 2026-06-02 23:39:34.134Z | 237.367° WSW |
| 10 mins | 2026-06-03 09:37:34.134Z | 142.201° SSE | 2026-06-03 09:41:34.134Z | 87.685° E | 34.206° | 2026-06-03 09:47:34.134Z | 13.887° NNE |
| 9 mins | 2026-06-03 11:23:34.134Z | 228.216° WSW | 2026-06-03 11:27:34.134Z | 275.903° WNW | 26.012° | 2026-06-03 11:32:34.134Z | 333.302° 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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