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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-32
1 61565U 24185P 26095.90857057 .00000141 00000-0 20082-3 0 9997
2 61565 88.9819 69.2235 0011809 92.3786 267.8717 13.50773017 83451Epoch: 2026-04-05T21:48Z
TLE epoch observation values (Epoch: 2026-04-05T21:48:20.497Z)
Latitude
-0.00003°
Longitude
-92.06915°
Altitude
1,072.706 km
Speed
7.315 km/s
True Right ascension
04h 36m 53s
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
11:25:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.259 km
Perigee altitude
1,057.676 km
Semi-major axis
7,444.604 km
Eccentricity
0.00118
Inclination
88.9819°
RAAN
69.2235°
Arg. of periapsis
92.3786°
True anomaly
267.73648°
Mean anomaly
267.8717°
Eccentric anomaly
267.80409°
Mean motion
3.37894 °/min
Orbital period
106.54 mins
BSTAR
0.00020082
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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 | 2026-04-06 09:05:25.796Z | 37.708° NE | 2026-04-06 09:09:25.796Z | 79.187° E | 19.044° | 2026-04-06 09:13:25.796Z | 119.571° SE |
| 11 mins | 2026-04-06 10:51:25.796Z | 350.947° N | 2026-04-06 10:56:25.796Z | 271.494° WNW | 41.624° | 2026-04-06 11:02:25.796Z | 197.107° SSW |
| 6 mins | 2026-04-06 21:05:25.796Z | 96.831° ESE | 2026-04-06 21:07:25.796Z | 75.779° E | 16.958° | 2026-04-06 21:11:25.796Z | 36.407° NE |
| 11 mins | 2026-04-06 22:48:25.796Z | 188.354° SSW | 2026-04-06 22:53:25.796Z | 266.551° W | 43.492° | 2026-04-06 22:59:25.796Z | 354.054° 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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