QIANFAN-167, 69384
Orbit data source: Space-Track
QIANFAN-167, 69384 is a Chinese payload satellite in LEO that was launched on Thu, 04 Jun 2026 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). 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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69384 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH
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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-167
1 69384U 26124C 26171.43142741 .00000083 00000-0 34650-4 0 9991
2 69384 88.9984 1.6718 0002273 151.4950 208.6363 14.16526392 2278Epoch: 2026-06-20T10:21Z
TLE epoch observation values (Epoch: 2026-06-20T10:21:15.328Z)
Latitude
0.00001°
Longitude
-62.28821°
Altitude
841.612 km
Speed
7.431 km/s
True Right ascension
00h 06m 41s
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
07:17:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
835.72 km
Perigee altitude
832.441 km
Semi-major axis
7,212.217 km
Eccentricity
0.00023
Inclination
88.9984°
RAAN
1.6718°
Arg. of periapsis
151.495°
True anomaly
208.62382°
Mean anomaly
208.6363°
Eccentric anomaly
208.63006°
Mean motion
3.54356 °/min
Orbital period
101.59 mins
BSTAR
0.00003465
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Other satellites on launch #124 in the year 2026 (2026-06-04 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-167 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 00:29:30.480Z | 14.221° NNE | 2026-06-21 00:34:30.480Z | 85.329° E | 35.648° | 2026-06-21 00:39:30.480Z | 158.604° S |
| 6 mins | 2026-06-21 02:13:30.480Z | 314.892° NW | 2026-06-21 02:15:30.480Z | 287.685° WNW | 19.813° | 2026-06-21 02:19:30.480Z | 237.993° WSW |
| 6 mins | 2026-06-21 11:56:30.480Z | 107.713° ESE | 2026-06-21 11:58:30.480Z | 81.512° E | 18.817° | 2026-06-21 12:02:30.480Z | 32.856° NE |
| 8 mins | 2026-06-21 13:36:30.480Z | 205.968° SW | 2026-06-21 13:40:30.480Z | 288.569° WNW | 36.495° | 2026-06-21 13:44:30.480Z | 344.51° N |
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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