QIANFAN-166, 69383
Orbit data source: Space-Track
QIANFAN-166, 69383 is a Chinese payload satellite in LEO that was launched on Thu, 04 Jun 2026 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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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69383 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
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-166
1 69383U 26124B 26171.43002942 .00000092 00000-0 38436-4 0 9994
2 69383 88.9985 1.6718 0002756 105.8734 254.2758 14.17059923 2274Epoch: 2026-06-20T10:19Z
TLE epoch observation values (Epoch: 2026-06-20T10:19:14.541Z)
Latitude
-0.00008°
Longitude
-61.78356°
Altitude
838.901 km
Speed
7.433 km/s
True Right ascension
00h 06m 41s
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
07:16:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
834.256 km
Perigee altitude
830.281 km
Semi-major axis
7,210.406 km
Eccentricity
0.00028
Inclination
88.9985°
RAAN
1.6718°
Arg. of periapsis
105.8734°
True anomaly
254.2454°
Mean anomaly
254.2758°
Eccentric anomaly
254.2606°
Mean motion
3.5449 °/min
Orbital period
101.55 mins
BSTAR
0.000038436
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Other satellites on launch #124 in the year 2026 (2026-06-04 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-166 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 00:27:36.344Z | 17.055° NNE | 2026-06-21 00:32:36.344Z | 98.766° ESE | 34.182° | 2026-06-21 00:36:36.344Z | 154.495° SSE |
| 6 mins | 2026-06-21 02:10:36.344Z | 321.184° NNW | 2026-06-21 02:13:36.344Z | 280.243° WNW | 20.683° | 2026-06-21 02:16:36.344Z | 241.27° WSW |
| 5 mins | 2026-06-21 11:54:36.344Z | 98.866° ESE | 2026-06-21 11:56:36.344Z | 71.479° E | 17.889° | 2026-06-21 11:59:36.344Z | 36.16° NE |
| 9 mins | 2026-06-21 13:33:36.344Z | 202.152° SSW | 2026-06-21 13:37:36.344Z | 279.635° WNW | 38.013° | 2026-06-21 13:42:36.344Z | 348.379° 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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