QIANFAN-195, 69413
Orbit data source: Space-Track
QIANFAN-195, 69413 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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69413 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-195
1 69413U 26125N 26170.77760962 -.02060440 00000-0 -10715+1 0 9991
2 69413 88.9935 280.1519 0014843 185.9073 174.1944 14.18838348 2073Epoch: 2026-06-19T18:39Z
TLE epoch observation values (Epoch: 2026-06-19T18:39:45.471Z)
Latitude
0.00002°
Longitude
92.21072°
Altitude
842.981 km
Speed
7.426 km/s
True Right ascension
18h 40m 36s
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
08:33:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
836.93 km
Perigee altitude
815.544 km
Semi-major axis
7,204.374 km
Eccentricity
0.00148
Inclination
88.9935°
RAAN
280.1519°
Arg. of periapsis
185.9073°
True anomaly
174.21157°
Mean anomaly
174.1944°
Eccentric anomaly
174.20299°
Mean motion
3.54935 °/min
Orbital period
101.43 mins
BSTAR
-1.0715
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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-195 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-21 06:26:02.459Z | 112.668° SE | 2026-06-21 06:29:02.459Z | 76.83° E | 17.869° | 2026-06-21 06:32:02.459Z | 40.209° NE |
| 8 mins | 2026-06-21 08:07:02.459Z | 202.549° SW | 2026-06-21 08:11:02.459Z | 291.669° WNW | 38.386° | 2026-06-21 08:15:02.459Z | 346.462° N |
| 8 mins | 2026-06-21 18:48:02.459Z | 29.729° NE | 2026-06-21 18:51:02.459Z | 75.897° E | 29.65° | 2026-06-21 18:56:02.459Z | 147.761° SSE |
| 7 mins | 2026-06-21 20:30:02.459Z | 327.98° NNW | 2026-06-21 20:33:02.459Z | 286.009° WNW | 24.975° | 2026-06-21 20:37:02.459Z | 230.135° WSW |
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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