QIANFAN-184, 69402
Orbit data source: Space-Track
QIANFAN-184, 69402 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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69402 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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-184
1 69402U 26125B 26171.15893426 -.01948538 00000-0 -11515+1 0 9995
2 69402 88.9945 280.1128 0020816 159.8124 200.3890 14.11639509 2121Epoch: 2026-06-20T03:48Z
TLE epoch observation values (Epoch: 2026-06-20T03:48:51.920Z)
Latitude
0.00008°
Longitude
-45.4811°
Altitude
870.925 km
Speed
7.41 km/s
True Right ascension
18h 40m 27s
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
08:32:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
865.778 km
Perigee altitude
835.682 km
Semi-major axis
7,228.867 km
Eccentricity
0.00208
Inclination
88.9945°
RAAN
280.1128°
Arg. of periapsis
159.8124°
True anomaly
200.3061°
Mean anomaly
200.389°
Eccentric anomaly
200.34753°
Mean motion
3.53133 °/min
Orbital period
101.94 mins
BSTAR
-1.1515
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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-184 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-06-21 07:10:59.242Z | 156.118° SSE | 2026-06-21 07:15:59.242Z | 91.017° ESE | 37.163° | 2026-06-21 07:20:59.242Z | 12.326° NNE |
| 6 mins | 2026-06-21 08:55:59.242Z | 244.247° WSW | 2026-06-21 08:58:59.242Z | 282.962° WNW | 19.495° | 2026-06-21 09:01:59.242Z | 319.803° NNW |
| 9 mins | 2026-06-21 19:37:59.242Z | 357.936° N | 2026-06-21 19:41:59.242Z | 252.343° W | 44.664° | 2026-06-21 19:46:59.242Z | 186.374° SSW |
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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