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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-32
1 61565U 24185P 26197.83596683 .00000108 00000-0 14884-3 0 9993
2 61565 88.9834 58.7827 0010257 151.1371 209.0350 13.50792791 97218Epoch: 2026-07-16T20:03Z
TLE epoch observation values (Epoch: 2026-07-16T20:03:47.534Z)
Latitude
0.00006°
Longitude
-176.83707°
Altitude
1,078.978 km
Speed
7.309 km/s
True Right ascension
03h 55m 07s
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
20:52:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.03 km
Perigee altitude
1,058.759 km
Semi-major axis
7,444.532 km
Eccentricity
0.00103
Inclination
88.9834°
RAAN
58.7827°
Arg. of periapsis
151.1371°
True anomaly
208.97802°
Mean anomaly
209.035°
Eccentric anomaly
209.0065°
Mean motion
3.37899 °/min
Orbital period
106.54 mins
BSTAR
0.00014884
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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 | 2026-07-17 13:57:53.194Z | 126.468° SE | 2026-07-17 14:02:53.194Z | 75.643° E | 22.806° | 2026-07-17 14:07:53.194Z | 25.289° NE |
| 11 mins | 2026-07-17 15:43:53.194Z | 201.825° SSW | 2026-07-17 15:48:53.194Z | 270.725° WNW | 38.263° | 2026-07-17 15:54:53.194Z | 347.748° N |
| 11 mins | 2026-07-18 02:53:53.194Z | 5.829° NNE | 2026-07-18 02:58:53.194Z | 118.348° SE | 44.145° | 2026-07-18 03:04:53.194Z | 176.712° S |
| 6 mins | 2026-07-18 04:41:53.194Z | 312.477° NW | 2026-07-18 04:43:53.194Z | 292.558° NW | 15.507° | 2026-07-18 04:47:53.194Z | 253.977° W |
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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