QIANFAN-177, 69394
Orbit data source: Space-Track
QIANFAN-177, 69394 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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69394 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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-177
1 69394U 26124N 26171.46798762 .00000065 00000-0 22466-4 0 9997
2 69394 88.9983 1.6587 0003879 137.6601 222.4890 14.22730564 2289Epoch: 2026-06-20T11:13Z
TLE epoch observation values (Epoch: 2026-06-20T11:13:54.130Z)
Latitude
-0.00007°
Longitude
-75.49903°
Altitude
821.249 km
Speed
7.441 km/s
True Right ascension
00h 06m 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
07:13:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
815.87 km
Perigee altitude
810.291 km
Semi-major axis
7,191.217 km
Eccentricity
0.00039
Inclination
88.9983°
RAAN
1.6587°
Arg. of periapsis
137.6601°
True anomaly
222.45899°
Mean anomaly
222.489°
Eccentric anomaly
222.47399°
Mean motion
3.55909 °/min
Orbital period
101.15 mins
BSTAR
0.000022466
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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-177 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 23:39:30.606Z | 50.477° ENE | 2026-06-20 23:41:30.606Z | 74.154° E | 14.399° | 2026-06-20 23:44:30.606Z | 109.455° ESE |
| 9 mins | 2026-06-21 01:19:30.606Z | 350.981° N | 2026-06-21 01:23:30.606Z | 270.303° WNW | 41.675° | 2026-06-21 01:28:30.606Z | 195.128° SSW |
| 9 mins | 2026-06-21 12:40:30.606Z | 153.401° SSE | 2026-06-21 12:44:30.606Z | 78.685° E | 37.741° | 2026-06-21 12:49:30.606Z | 9.942° NNE |
| 6 mins | 2026-06-21 14:23:30.606Z | 249.543° W | 2026-06-21 14:25:30.606Z | 275.349° WNW | 17.534° | 2026-06-21 14:29:30.606Z | 323.781° NNW |
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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