QIANFAN-32, 61565
Orbit data source: Space-Track
QIANFAN-32, 61565 is a Chinese payload satellite in LEO that was launched on Tue, 15 Oct 2024 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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61565 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH/SECM
Mission
Operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-32
1 61565U 24185P 26315.61339912 .00000188 00000-0 27327-3 0 9995
2 61565 88.9932 46.7236 0010038 173.3795 186.7490 13.50825201113118Epoch: 2026-11-11T14:43Z
TLE epoch observation values (Epoch: 2026-11-11T14:43:17.683Z)
Latitude
-0.0001°
Longitude
135.14119°
Altitude
1,079.602 km
Speed
7.309 km/s
True Right ascension
03h 06m 53s
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
20:26:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.748 km
Perigee altitude
1,058.803 km
Semi-major axis
7,444.412 km
Eccentricity
0.001
Inclination
88.9932°
RAAN
46.7236°
Arg. of periapsis
173.3795°
True anomaly
186.7355°
Mean anomaly
186.749°
Eccentric anomaly
186.74225°
Mean motion
3.37907 °/min
Orbital period
106.54 mins
BSTAR
0.00027327
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Other satellites on launch #185 in the year 2024 (2024-10-15 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-32 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-12 05:05:59.331Z | 104.636° ESE | 2026-11-12 05:08:59.331Z | 75.996° E | 16.772° | 2026-11-12 05:12:59.331Z | 37.551° NE |
| 11 mins | 2026-11-12 06:49:59.331Z | 185.391° SSW | 2026-11-12 06:54:59.331Z | 262.777° W | 76.423° | 2026-11-12 07:00:59.331Z | 355.334° N |
| 11 mins | 2026-11-12 17:59:59.331Z | 16.058° NNE | 2026-11-12 18:04:59.331Z | 94.412° ESE | 52.622° | 2026-11-12 18:10:59.331Z | 162.567° S |
| 8 mins | 2026-11-12 19:46:59.331Z | 326.869° NNW | 2026-11-12 19:50:59.331Z | 282.184° WNW | 24.323° | 2026-11-12 19:54:59.331Z | 239.311° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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