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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-32
1 61565U 24185P 25305.64294707 .00000193 00000-0 28137-3 0 9994
2 61565 88.9819 85.1821 0009700 172.1074 188.0231 13.50717026 62497Epoch: 2025-11-01T15:25Z
TLE epoch observation values (Epoch: 2025-11-01T15:25:50.626Z)
Latitude
-0.00008°
Longitude
172.55107°
Altitude
1,079.73 km
Speed
7.309 km/s
True Right ascension
05h 40m 43s
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
05:41:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.895 km
Perigee altitude
1,059.452 km
Semi-major axis
7,444.81 km
Eccentricity
0.00097
Inclination
88.9819°
RAAN
85.1821°
Arg. of periapsis
172.1074°
True anomaly
188.0076°
Mean anomaly
188.0231°
Eccentric anomaly
188.01535°
Mean motion
3.3788 °/min
Orbital period
106.55 mins
BSTAR
0.00028137
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-02 11:06:24.943Z | 229.217° WSW | 2025-11-02 11:11:24.943Z | 280.769° WNW | 22.683° | 2025-11-02 11:16:24.943Z | 331.949° NNW |
| 8 mins | 2025-11-02 20:30:24.943Z | 39.851° NE | 2025-11-02 20:33:24.943Z | 74.538° E | 22.739° | 2025-11-02 20:38:24.943Z | 129.188° SE |
| 11 mins | 2025-11-02 22:15:24.943Z | 347.184° N | 2025-11-02 22:20:24.943Z | 283.612° WNW | 37.789° | 2025-11-02 22:26:24.943Z | 205.261° SW |
| 8 mins | 2025-11-03 08:28:24.943Z | 112.181° ESE | 2025-11-03 08:31:24.943Z | 80.111° E | 20.596° | 2025-11-03 08:36:24.943Z | 29.093° NE |
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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