QIANFAN-189, 69407
Orbit data source: Space-Track
QIANFAN-189, 69407 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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69407 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-189
1 69407U 26125G 26170.72193317 -.01853945 00000-0 -10384+1 0 9994
2 69407 88.9947 280.1586 0014980 167.6028 192.5531 14.14417547 2067Epoch: 2026-06-19T17:19Z
TLE epoch observation values (Epoch: 2026-06-19T17:19:35.025Z)
Latitude
0°
Longitude
112.31583°
Altitude
857.903 km
Speed
7.418 km/s
True Right ascension
18h 40m 38s
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
08:32:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
852.068 km
Perigee altitude
830.439 km
Semi-major axis
7,219.391 km
Eccentricity
0.0015
Inclination
88.9947°
RAAN
280.1586°
Arg. of periapsis
167.6028°
True anomaly
192.51586°
Mean anomaly
192.5531°
Eccentric anomaly
192.53447°
Mean motion
3.53828 °/min
Orbital period
101.74 mins
BSTAR
-1.0384
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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-189 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-21 06:52:48.449Z | 139.139° SSE | 2026-06-21 06:56:48.449Z | 87.64° E | 28.672° | 2026-06-21 07:01:48.449Z | 19.822° NNE |
| 8 mins | 2026-06-21 08:35:48.449Z | 225.772° WSW | 2026-06-21 08:39:48.449Z | 286.397° WNW | 26.45° | 2026-06-21 08:43:48.449Z | 335.174° NNW |
| 9 mins | 2026-06-21 19:17:48.449Z | 9.702° NNE | 2026-06-21 19:21:48.449Z | 82.801° E | 42.606° | 2026-06-21 19:26:48.449Z | 171.005° S |
| 4 mins | 2026-06-21 21:01:48.449Z | 307.226° NW | 2026-06-21 21:03:48.449Z | 283.513° WNW | 14.625° | 2026-06-21 21:05:48.449Z | 260.576° W |
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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