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: 15 hours ago
TLE from 15 hours ago
0 QIANFAN-32
1 61565U 24185P 25350.31216179 .00000085 00000-0 11370-3 0 9996
2 61565 88.9854 80.6045 0010685 60.9969 299.2252 13.50736143 68524Epoch: 2025-12-16T07:29Z
TLE epoch observation values (Epoch: 2025-12-16T07:29:30.778Z)
Latitude
0.00001°
Longitude
-116.97192°
Altitude
1,068.624 km
Speed
7.32 km/s
True Right ascension
05h 22m 25s
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
21:16:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.558 km
Perigee altitude
1,058.648 km
Semi-major axis
7,444.74 km
Eccentricity
0.00107
Inclination
88.9854°
RAAN
80.6045°
Arg. of periapsis
60.9969°
True anomaly
299.11828°
Mean anomaly
299.2252°
Eccentric anomaly
299.17174°
Mean motion
3.37885 °/min
Orbital period
106.55 mins
BSTAR
0.0001137
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-17 04:59:47.758Z | 96.663° ESE | 2025-12-17 05:02:47.758Z | 66.888° ENE | 14.791° | 2025-12-17 05:05:47.758Z | 39.197° NE |
| 11 mins | 2025-12-17 06:42:47.758Z | 182.481° SSW | 2025-12-17 06:47:47.758Z | 239.452° WSW | 44.529° | 2025-12-17 06:53:47.758Z | 356.552° N |
| 11 mins | 2025-12-17 17:52:47.758Z | 17.108° NNE | 2025-12-17 17:57:47.758Z | 90.482° ESE | 37.296° | 2025-12-17 18:03:47.758Z | 160.077° S |
| 9 mins | 2025-12-17 19:39:47.758Z | 328.738° NNW | 2025-12-17 19:43:47.758Z | 283.747° WNW | 23.614° | 2025-12-17 19:48:47.758Z | 232.079° WSW |
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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