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 26045.61085308 .00000143 00000-0 20410-3 0 9999
2 61565 88.9786 74.4077 0008055 231.1633 128.8799 13.50758637 76661Epoch: 2026-02-14T14:39Z
TLE epoch observation values (Epoch: 2026-02-14T14:39:37.706Z)
Latitude
-0.00006°
Longitude
69.86916°
Altitude
1,076.191 km
Speed
7.312 km/s
True Right ascension
04h 57m 37s
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
02:32:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,072.517 km
Perigee altitude
1,060.523 km
Semi-major axis
7,444.657 km
Eccentricity
0.00081
Inclination
88.9786°
RAAN
74.4077°
Arg. of periapsis
231.1633°
True anomaly
128.95171°
Mean anomaly
128.8799°
Eccentric anomaly
128.91581°
Mean motion
3.37891 °/min
Orbital period
106.54 mins
BSTAR
0.0002041
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-02-15 01:26:34.655Z | 141.957° SSE | 2026-02-15 01:31:34.655Z | 83.656° E | 31.9° | 2026-02-15 01:37:34.655Z | 15.689° NNE |
| 10 mins | 2026-02-15 03:13:34.655Z | 220.748° SW | 2026-02-15 03:18:34.655Z | 282.483° WNW | 28.795° | 2026-02-15 03:23:34.655Z | 337.432° NNW |
| 7 mins | 2026-02-15 12:37:34.655Z | 44.879° NE | 2026-02-15 12:40:34.655Z | 75.721° E | 17.418° | 2026-02-15 12:44:34.655Z | 115.231° SE |
| 11 mins | 2026-02-15 14:22:34.655Z | 354.033° N | 2026-02-15 14:27:34.655Z | 288.789° WNW | 42.99° | 2026-02-15 14:33:34.655Z | 193.865° SSW |
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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