QIANFAN-200, 69418
Orbit data source: Space-Track
QIANFAN-200, 69418 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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69418 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-200
1 69418U 26125T 26170.85805584 -.01893052 00000-0 -10402+1 0 9990
2 69418 88.9946 280.1421 0014564 173.5980 186.5397 14.15539357 2087Epoch: 2026-06-19T20:35Z
TLE epoch observation values (Epoch: 2026-06-19T20:35:36.024Z)
Latitude
0.00003°
Longitude
63.161°
Altitude
853.972 km
Speed
7.42 km/s
True Right ascension
18h 40m 34s
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
07:12:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.944 km
Perigee altitude
826.927 km
Semi-major axis
7,215.573 km
Eccentricity
0.00146
Inclination
88.9946°
RAAN
280.1421°
Arg. of periapsis
173.598°
True anomaly
186.52073°
Mean anomaly
186.5397°
Eccentric anomaly
186.53021°
Mean motion
3.54109 °/min
Orbital period
101.66 mins
BSTAR
-1.0402
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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-200 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 20:59:08.660Z | 316.167° NNW | 2026-06-20 21:02:08.660Z | 279.64° WNW | 16.133° | 2026-06-20 21:04:08.660Z | 255.756° W |
| 7 mins | 2026-06-21 06:44:08.660Z | 122.315° SE | 2026-06-21 06:47:08.660Z | 78.913° E | 24.619° | 2026-06-21 06:51:08.660Z | 27.055° NE |
| 9 mins | 2026-06-21 08:25:08.660Z | 215.354° SW | 2026-06-21 08:29:08.660Z | 277.211° WNW | 31.023° | 2026-06-21 08:34:08.660Z | 341.781° N |
| 9 mins | 2026-06-21 19:07:08.660Z | 16.597° NNE | 2026-06-21 19:11:08.660Z | 92.823° ESE | 38.588° | 2026-06-21 19:16:08.660Z | 163.557° 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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