QIANFAN-197, 69415
Orbit data source: Space-Track
QIANFAN-197, 69415 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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69415 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-197
1 69415U 26125Q 26170.77375360 -.01921916 00000-0 -10034+1 0 9994
2 69415 88.9949 280.1479 0009001 172.9343 187.1975 14.18379903 2065Epoch: 2026-06-19T18:34Z
TLE epoch observation values (Epoch: 2026-06-19T18:34:12.311Z)
Latitude
0.00003°
Longitude
93.59869°
Altitude
840.327 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
07:11:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
834.277 km
Perigee altitude
821.305 km
Semi-major axis
7,205.928 km
Eccentricity
0.0009
Inclination
88.9949°
RAAN
280.1479°
Arg. of periapsis
172.9343°
True anomaly
187.18459°
Mean anomaly
187.1975°
Eccentric anomaly
187.19104°
Mean motion
3.5482 °/min
Orbital period
101.46 mins
BSTAR
-1.0034
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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-197 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 20:35:14.782Z | 335.485° NNW | 2026-06-20 20:39:14.782Z | 287.568° WNW | 23.944° | 2026-06-20 20:43:14.782Z | 231.909° WSW |
| 5 mins | 2026-06-21 06:22:14.782Z | 96.503° ESE | 2026-06-21 06:24:14.782Z | 71.37° E | 16.069° | 2026-06-21 06:27:14.782Z | 37.908° NE |
| 9 mins | 2026-06-21 08:01:14.782Z | 195.209° SSW | 2026-06-21 08:05:14.782Z | 266.28° W | 40.957° | 2026-06-21 08:10:14.782Z | 350.203° N |
| 7 mins | 2026-06-21 18:43:14.782Z | 36.389° NE | 2026-06-21 18:46:14.782Z | 85.821° E | 27.63° | 2026-06-21 18:50:14.782Z | 140.957° 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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