QIANFAN-196, 69414
Orbit data source: Space-Track
QIANFAN-196, 69414 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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69414 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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-196
1 69414U 26125P 26171.40753214 -.01762764 00000-0 -93611+0 0 9997
2 69414 88.9949 280.0754 0014385 184.6406 175.4652 14.17746327 2160Epoch: 2026-06-20T09:46Z
TLE epoch observation values (Epoch: 2026-06-20T09:46:50.776Z)
Latitude
-0.00004°
Longitude
-135.25876°
Altitude
846.377 km
Speed
7.424 km/s
True Right ascension
18h 40m 18s
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
08:32:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
840.308 km
Perigee altitude
819.57 km
Semi-major axis
7,208.076 km
Eccentricity
0.00144
Inclination
88.9949°
RAAN
280.0754°
Arg. of periapsis
184.6406°
True anomaly
175.47821°
Mean anomaly
175.4652°
Eccentric anomaly
175.47171°
Mean motion
3.54662 °/min
Orbital period
101.51 mins
BSTAR
-0.93611
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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-196 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 | 2026-06-21 06:17:33.463Z | 100.579° ESE | 2026-06-21 06:19:33.463Z | 77.558° E | 14.729° | 2026-06-21 06:22:33.463Z | 43.27° NE |
| 9 mins | 2026-06-21 07:56:33.463Z | 190.509° SSW | 2026-06-21 08:00:33.463Z | 243.877° WSW | 41.855° | 2026-06-21 08:05:33.463Z | 351.346° N |
| 7 mins | 2026-06-21 18:37:33.463Z | 34.691° NE | 2026-06-21 18:40:33.463Z | 77.722° E | 25.162° | 2026-06-21 18:44:33.463Z | 134.746° SE |
| 8 mins | 2026-06-21 20:19:33.463Z | 331.101° NNW | 2026-06-21 20:22:33.463Z | 283.155° WNW | 29.356° | 2026-06-21 20:27:33.463Z | 216.355° SW |
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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