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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-32
1 61565U 24185P 26135.24261937 .00000116 00000-0 16226-3 0 9992
2 61565 88.9869 65.1925 0009678 354.4922 5.6121 13.50782204 88766Epoch: 2026-05-15T05:49Z
TLE epoch observation values (Epoch: 2026-05-15T05:49:22.313Z)
Latitude
-0.00003°
Longitude
104.87279°
Altitude
1,065.16 km
Speed
7.323 km/s
True Right ascension
04h 20m 46s
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
08:19:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.638 km
Perigee altitude
1,059.229 km
Semi-major axis
7,444.57 km
Eccentricity
0.00097
Inclination
88.9869°
RAAN
65.1925°
Arg. of periapsis
354.4922°
True anomaly
5.62296°
Mean anomaly
5.6121°
Eccentric anomaly
5.61753°
Mean motion
3.37897 °/min
Orbital period
106.54 mins
BSTAR
0.00016226
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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 | 2026-05-16 07:18:13.189Z | 7.019° NNE | 2026-05-16 07:24:13.189Z | 90.728° ESE | 42.861° | 2026-05-16 07:30:13.189Z | 171.22° S |
| 7 mins | 2026-05-16 09:07:13.189Z | 316.307° NNW | 2026-05-16 09:10:13.189Z | 284.492° WNW | 18.074° | 2026-05-16 09:14:13.189Z | 246.141° WSW |
| 11 mins | 2026-05-16 19:16:13.189Z | 158.431° S | 2026-05-16 19:21:13.189Z | 86.369° E | 40.728° | 2026-05-16 19:27:13.189Z | 7.857° NNE |
| 7 mins | 2026-05-16 21:05:13.189Z | 247.745° W | 2026-05-16 21:08:13.189Z | 281.282° WNW | 20.045° | 2026-05-16 21:12:13.189Z | 323.377° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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