QIANFAN-180, 69397
Orbit data source: Space-Track
QIANFAN-180, 69397 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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69397 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-180
1 69397U 26124R 26171.46417792 .00000066 00000-0 22696-4 0 9997
2 69397 88.9983 1.6582 0003330 154.3492 205.7866 14.23618729 2289Epoch: 2026-06-20T11:08Z
TLE epoch observation values (Epoch: 2026-06-20T11:08:24.972Z)
Latitude
0°
Longitude
-74.12428°
Altitude
818.356 km
Speed
7.443 km/s
True Right ascension
00h 06m 37s
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
07:12:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
812.48 km
Perigee altitude
807.693 km
Semi-major axis
7,188.224 km
Eccentricity
0.00033
Inclination
88.9983°
RAAN
1.6582°
Arg. of periapsis
154.3492°
True anomaly
205.77001°
Mean anomaly
205.7866°
Eccentric anomaly
205.7783°
Mean motion
3.56132 °/min
Orbital period
101.09 mins
BSTAR
0.000022696
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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-180 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 01:13:18.357Z | 354.872° N | 2026-06-21 01:17:18.357Z | 287.813° WNW | 43.441° | 2026-06-21 01:22:18.357Z | 190.992° SSW |
| 8 mins | 2026-06-21 12:34:18.357Z | 146.98° SSE | 2026-06-21 12:38:18.357Z | 72.498° E | 34.576° | 2026-06-21 12:42:18.357Z | 15.445° NNE |
| 5 mins | 2026-06-21 14:17:18.357Z | 250.416° W | 2026-06-21 14:19:18.357Z | 279.434° WNW | 19.862° | 2026-06-21 14:22:18.357Z | 319.472° 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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