QIANFAN-188, 69406
Orbit data source: Space-Track
QIANFAN-188, 69406 is a Chinese payload satellite in LEO that was launched on Fri, 05 Jun 2026 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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69406 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
SECM?
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: 1 day ago
TLE from 1 day ago
0 QIANFAN-188
1 69406U 26125F 26170.79316292 -.02077050 00000-0 -11264+1 0 9993
2 69406 88.9989 280.1491 0017376 182.4114 177.6993 14.16598732 2075Epoch: 2026-06-19T19:02Z
TLE epoch observation values (Epoch: 2026-06-19T19:02:09.276Z)
Latitude
-0.00005°
Longitude
86.59341°
Altitude
852.456 km
Speed
7.42 km/s
True Right ascension
18h 40m 35s
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
07:15:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
846.366 km
Perigee altitude
821.303 km
Semi-major axis
7,211.972 km
Eccentricity
0.00174
Inclination
88.9989°
RAAN
280.1491°
Arg. of periapsis
182.4114°
True anomaly
177.70728°
Mean anomaly
177.6993°
Eccentric anomaly
177.70329°
Mean motion
3.54374 °/min
Orbital period
101.59 mins
BSTAR
-1.1264
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Other satellites on launch #125 in the year 2026 (2026-06-05 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-188 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 21:07:11.637Z | 311.126° NW | 2026-06-20 21:09:11.637Z | 288.313° WNW | 13.859° | 2026-06-20 21:11:11.637Z | 264.913° W |
| 8 mins | 2026-06-21 06:51:11.637Z | 131.535° SE | 2026-06-21 06:54:11.637Z | 89.855° E | 27.428° | 2026-06-21 06:59:11.637Z | 21.395° NNE |
| 8 mins | 2026-06-21 08:33:11.637Z | 224.112° SW | 2026-06-21 08:36:11.637Z | 266.345° W | 27.467° | 2026-06-21 08:41:11.637Z | 336.132° NNW |
| 9 mins | 2026-06-21 19:14:11.637Z | 10.657° NNE | 2026-06-21 19:18:11.637Z | 68.65° E | 41.099° | 2026-06-21 19:23:11.637Z | 167.768° S |
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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