QIANFAN-178, 69395
Orbit data source: Space-Track
QIANFAN-178, 69395 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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69395 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-178
1 69395U 26124P 26171.46966823 .00000260 00000-0 11053-3 0 9999
2 69395 88.9983 1.6589 0003089 146.3393 213.7995 14.22274602 2285Epoch: 2026-06-20T11:16Z
TLE epoch observation values (Epoch: 2026-06-20T11:16:19.335Z)
Latitude
-0°
Longitude
-76.1055°
Altitude
822.575 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
07:17:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
816.84 km
Perigee altitude
812.397 km
Semi-major axis
7,192.755 km
Eccentricity
0.00031
Inclination
88.9983°
RAAN
1.6589°
Arg. of periapsis
146.3393°
True anomaly
213.77982°
Mean anomaly
213.7995°
Eccentric anomaly
213.78966°
Mean motion
3.55795 °/min
Orbital period
101.18 mins
BSTAR
0.00011053
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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-178 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 23:41:42.293Z | 45.136° ENE | 2026-06-20 23:44:42.293Z | 81.1° E | 15.288° | 2026-06-20 23:46:42.293Z | 105.556° ESE |
| 8 mins | 2026-06-21 01:22:42.293Z | 347.4° N | 2026-06-21 01:25:42.293Z | 296.627° NW | 40.11° | 2026-06-21 01:30:42.293Z | 198.292° SSW |
| 8 mins | 2026-06-21 12:43:42.293Z | 154.456° SSE | 2026-06-21 12:47:42.293Z | 65.765° ENE | 38.506° | 2026-06-21 12:51:42.293Z | 10.878° NNE |
| 5 mins | 2026-06-21 14:26:42.293Z | 253.423° W | 2026-06-21 14:28:42.293Z | 279.102° WNW | 16.676° | 2026-06-21 14:31:42.293Z | 316.195° 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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