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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-32
1 61565U 24185P 26304.20615024 .00000148 00000-0 21136-3 0 9997
2 61565 88.9925 47.8837 0008980 205.6190 154.4517 13.50820334111572Epoch: 2026-10-31T04:56Z
TLE epoch observation values (Epoch: 2026-10-31T04:56:51.380Z)
Latitude
-0.00006°
Longitude
-65.84559°
Altitude
1,078.231 km
Speed
7.31 km/s
True Right ascension
03h 11m 32s
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
06:34:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,072.978 km
Perigee altitude
1,059.608 km
Semi-major axis
7,444.43 km
Eccentricity
0.0009
Inclination
88.9925°
RAAN
47.8837°
Arg. of periapsis
205.619°
True anomaly
154.49603°
Mean anomaly
154.4517°
Eccentric anomaly
154.47387°
Mean motion
3.37906 °/min
Orbital period
106.54 mins
BSTAR
0.00021136
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-10-31 18:00:32.989Z | 35.979° NE | 2026-10-31 18:04:32.989Z | 77.158° E | 21.159° | 2026-10-31 18:08:32.989Z | 119.143° SE |
| 11 mins | 2026-10-31 19:46:32.989Z | 350.428° N | 2026-10-31 19:51:32.989Z | 278.793° WNW | 60.491° | 2026-10-31 19:57:32.989Z | 198.837° SSW |
| 7 mins | 2026-11-01 05:59:32.989Z | 106.33° ESE | 2026-11-01 06:02:32.989Z | 76.046° E | 18.791° | 2026-11-01 06:06:32.989Z | 36.209° NE |
| 11 mins | 2026-11-01 07:43:32.989Z | 189.939° SSW | 2026-11-01 07:48:32.989Z | 266.371° W | 69.243° | 2026-11-01 07:54:32.989Z | 353.209° N |
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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