QIANFAN-176, 69393
Orbit data source: Space-Track
QIANFAN-176, 69393 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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69393 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-176
1 69393U 26124M 26171.47183025 .00000085 00000-0 32077-4 0 9998
2 69393 88.9983 1.6593 0002609 161.9704 198.1580 14.21841160 2288Epoch: 2026-06-20T11:19Z
TLE epoch observation values (Epoch: 2026-06-20T11:19:26.133Z)
Latitude
-0.00004°
Longitude
-76.88556°
Altitude
823.973 km
Speed
7.44 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
07:14:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
817.958 km
Perigee altitude
814.204 km
Semi-major axis
7,194.218 km
Eccentricity
0.00026
Inclination
88.9983°
RAAN
1.6593°
Arg. of periapsis
161.9704°
True anomaly
198.14869°
Mean anomaly
198.158°
Eccentric anomaly
198.15334°
Mean motion
3.55687 °/min
Orbital period
101.21 mins
BSTAR
0.000032077
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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-176 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 23:45:19.308Z | 47.011° ENE | 2026-06-20 23:48:19.308Z | 84.982° E | 16.292° | 2026-06-20 23:50:19.308Z | 109.587° ESE |
| 9 mins | 2026-06-21 01:25:19.308Z | 348.532° N | 2026-06-21 01:29:19.308Z | 283.099° WNW | 39.275° | 2026-06-21 01:34:19.308Z | 200.149° SSW |
| 8 mins | 2026-06-21 12:47:19.308Z | 157.506° S | 2026-06-21 12:51:19.308Z | 60.924° ENE | 39.776° | 2026-06-21 12:55:19.308Z | 9.05° NNE |
| 5 mins | 2026-06-21 14:30:19.308Z | 254.7° W | 2026-06-21 14:32:19.308Z | 279.348° WNW | 15.546° | 2026-06-21 14:35:19.308Z | 315.294° 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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