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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Edit Public Description
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: 16 hours ago
TLE from 16 hours ago
0 QIANFAN-32
1 61565U 24185P 25319.79198316 .00000225 00000-0 33039-3 0 9997
2 61565 88.9837 83.7303 0010792 135.7034 224.4982 13.50722358 64405Epoch: 2025-11-15T19:00Z
TLE epoch observation values (Epoch: 2025-11-15T19:00:27.345Z)
Latitude
-0.00005°
Longitude
103.50031°
Altitude
1,078.293 km
Speed
7.31 km/s
True Right ascension
05h 34m 55s
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
07:33:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.688 km
Perigee altitude
1,058.619 km
Semi-major axis
7,444.791 km
Eccentricity
0.00108
Inclination
88.9837°
RAAN
83.7303°
Arg. of periapsis
135.7034°
True anomaly
224.41161°
Mean anomaly
224.4982°
Eccentric anomaly
224.45489°
Mean motion
3.37882 °/min
Orbital period
106.55 mins
BSTAR
0.00033039
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-16 20:29:32.054Z | 5.24° NNE | 2025-11-16 20:35:32.054Z | 107.317° ESE | 43.877° | 2025-11-16 20:41:32.054Z | 175.159° S |
| 6 mins | 2025-11-16 22:18:32.054Z | 313.652° NW | 2025-11-16 22:21:32.054Z | 282.656° WNW | 16.128° | 2025-11-16 22:24:32.054Z | 253.937° W |
| 11 mins | 2025-11-17 08:27:32.054Z | 162.277° S | 2025-11-17 08:32:32.054Z | 81.151° E | 42.346° | 2025-11-17 08:38:32.054Z | 5.779° NNE |
| 7 mins | 2025-11-17 10:16:32.054Z | 250.628° W | 2025-11-17 10:19:32.054Z | 282.542° WNW | 18.364° | 2025-11-17 10:23:32.054Z | 322.691° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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