QIANFAN-198, 69416
Orbit data source: Space-Track
QIANFAN-198, 69416 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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69416 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-198
1 69416U 26125R 26170.77438195 -.01897356 00000-0 -99690+0 0 9995
2 69416 88.9948 280.1483 0009053 170.9232 189.2123 14.17990071 2075Epoch: 2026-06-19T18:35Z
TLE epoch observation values (Epoch: 2026-06-19T18:35:06.600Z)
Latitude
0.00005°
Longitude
93.37227°
Altitude
841.653 km
Speed
7.429 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
07:14:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
835.637 km
Perigee altitude
822.588 km
Semi-major axis
7,207.249 km
Eccentricity
0.00091
Inclination
88.9948°
RAAN
280.1483°
Arg. of periapsis
170.9232°
True anomaly
189.19571°
Mean anomaly
189.2123°
Eccentric anomaly
189.204°
Mean motion
3.54723 °/min
Orbital period
101.49 mins
BSTAR
-0.9969
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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-198 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 20:37:15.572Z | 329.974° NNW | 2026-06-20 20:41:15.572Z | 274.802° WNW | 23.427° | 2026-06-20 20:45:15.572Z | 227.588° WSW |
| 5 mins | 2026-06-21 06:23:15.572Z | 101.569° ESE | 2026-06-21 06:25:15.572Z | 76.929° E | 16.573° | 2026-06-21 06:28:15.572Z | 41.311° NE |
| 9 mins | 2026-06-21 08:03:15.572Z | 198.893° SSW | 2026-06-21 08:07:15.572Z | 293.144° NW | 39.838° | 2026-06-21 08:12:15.572Z | 351.036° N |
| 8 mins | 2026-06-21 18:44:15.572Z | 30.271° NE | 2026-06-21 18:47:15.572Z | 73.45° E | 28.008° | 2026-06-21 18:52:15.572Z | 144.62° SSE |
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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