QIANFAN-171, 69388
Orbit data source: Space-Track
QIANFAN-171, 69388 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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69388 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-171
1 69388U 26124G 26171.41171138 .00000371 00000-0 16761-3 0 9997
2 69388 88.9984 1.6688 0002320 168.1742 191.9503 14.20068413 2275Epoch: 2026-06-20T09:52Z
TLE epoch observation values (Epoch: 2026-06-20T09:52:51.863Z)
Latitude
-0.00001°
Longitude
-55.17401°
Altitude
829.81 km
Speed
7.437 km/s
True Right ascension
00h 06m 40s
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
07:13:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
823.743 km
Perigee altitude
820.402 km
Semi-major axis
7,200.21 km
Eccentricity
0.00023
Inclination
88.9984°
RAAN
1.6688°
Arg. of periapsis
168.1742°
True anomaly
191.9448°
Mean anomaly
191.9503°
Eccentric anomaly
191.94755°
Mean motion
3.55243 °/min
Orbital period
101.34 mins
BSTAR
0.00016761
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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-171 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-20 23:59:39.789Z | 29.076° NE | 2026-06-21 00:03:39.789Z | 78.215° E | 22.153° | 2026-06-21 00:07:39.789Z | 131.074° SE |
| 8 mins | 2026-06-21 01:41:39.789Z | 338.313° N | 2026-06-21 01:45:39.789Z | 269.442° W | 32.073° | 2026-06-21 01:49:39.789Z | 213.947° SW |
| 9 mins | 2026-06-21 13:03:39.789Z | 174.443° S | 2026-06-21 13:07:39.789Z | 64.221° ENE | 44.832° | 2026-06-21 13:12:39.789Z | 0.583° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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