QIANFAN-174, 69391
Orbit data source: Space-Track
QIANFAN-174, 69391 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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69391 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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-174
1 69391U 26124K 26171.47596933 .00000106 00000-0 42176-4 0 9997
2 69391 88.9983 1.6599 0003176 142.8570 217.2841 14.20878413 2284Epoch: 2026-06-20T11:25Z
TLE epoch observation values (Epoch: 2026-06-20T11:25:23.750Z)
Latitude
0.00002°
Longitude
-78.37911°
Altitude
827.258 km
Speed
7.438 km/s
True Right ascension
00h 06m 38s
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
07:15:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
821.619 km
Perigee altitude
817.048 km
Semi-major axis
7,197.471 km
Eccentricity
0.00032
Inclination
88.9983°
RAAN
1.6599°
Arg. of periapsis
142.857°
True anomaly
217.26206°
Mean anomaly
217.2841°
Eccentric anomaly
217.27308°
Mean motion
3.55446 °/min
Orbital period
101.28 mins
BSTAR
0.000042176
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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-174 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-20 23:51:06.479Z | 38.654° NE | 2026-06-20 23:54:06.479Z | 75.565° E | 18.602° | 2026-06-20 23:58:06.479Z | 124.776° SE |
| 9 mins | 2026-06-21 01:32:06.479Z | 343.961° N | 2026-06-21 01:36:06.479Z | 271.973° WNW | 36.495° | 2026-06-21 01:41:06.479Z | 203.924° SW |
| 9 mins | 2026-06-21 12:54:06.479Z | 164.807° S | 2026-06-21 12:58:06.479Z | 62.891° ENE | 42.618° | 2026-06-21 13:03:06.479Z | 4.429° NNE |
| 4 mins | 2026-06-21 14:38:06.479Z | 264.601° W | 2026-06-21 14:40:06.479Z | 288.531° WNW | 13.35° | 2026-06-21 14:42:06.479Z | 310.931° 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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