QIANFAN-190, 69408
Orbit data source: Space-Track
QIANFAN-190, 69408 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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69408 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: 23 hours ago
TLE from 23 hours ago
0 QIANFAN-190
1 69408U 26125H 26170.93298204 -.02091624 00000-0 -11418+1 0 9997
2 69408 88.9967 280.1343 0017438 185.5805 174.5192 14.16273042 2092Epoch: 2026-06-19T22:23Z
TLE epoch observation values (Epoch: 2026-06-19T22:23:29.648Z)
Latitude
0.00004°
Longitude
36.10591°
Altitude
853.561 km
Speed
7.419 km/s
True Right ascension
18h 40m 32s
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
08:33:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.519 km
Perigee altitude
822.363 km
Semi-major axis
7,213.078 km
Eccentricity
0.00174
Inclination
88.9967°
RAAN
280.1343°
Arg. of periapsis
185.5805°
True anomaly
174.53824°
Mean anomaly
174.5192°
Eccentric anomaly
174.52873°
Mean motion
3.54293 °/min
Orbital period
101.61 mins
BSTAR
-1.1418
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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-190 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 06:47:51.909Z | 135.994° SSE | 2026-06-21 06:51:51.909Z | 86.437° E | 26.555° | 2026-06-21 06:56:51.909Z | 21.411° NNE |
| 8 mins | 2026-06-21 08:30:51.909Z | 223.902° SW | 2026-06-21 08:33:51.909Z | 269.398° W | 28.724° | 2026-06-21 08:38:51.909Z | 338.06° N |
| 9 mins | 2026-06-21 19:11:51.909Z | 12.866° NNE | 2026-06-21 19:15:51.909Z | 82.727° E | 40.547° | 2026-06-21 19:20:51.909Z | 166.478° S |
| 5 mins | 2026-06-21 20:55:51.909Z | 307.482° NW | 2026-06-21 20:57:51.909Z | 282.209° WNW | 16.352° | 2026-06-21 21:00:51.909Z | 248.295° W |
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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