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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-32
1 61565U 24185P 25260.89902519 .00000180 00000-0 26083-3 0 9992
2 61565 88.9784 89.7883 0008076 319.3282 40.7265 13.50696408 56457Epoch: 2025-09-17T21:34Z
TLE epoch observation values (Epoch: 2025-09-17T21:34:35.776Z)
Latitude
-0.00003°
Longitude
129.07087°
Altitude
1,068.093 km
Speed
7.32 km/s
True Right ascension
05h 59m 09s
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
23:54:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,072.761 km
Perigee altitude
1,060.737 km
Semi-major axis
7,444.886 km
Eccentricity
0.00081
Inclination
88.9784°
RAAN
89.7883°
Arg. of periapsis
319.3282°
True anomaly
40.78693°
Mean anomaly
40.7265°
Eccentric anomaly
40.75671°
Mean motion
3.37875 °/min
Orbital period
106.55 mins
BSTAR
0.00026083
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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 | 2025-09-18 11:55:33.620Z | 126.588° SE | 2025-09-18 12:00:33.620Z | 73.169° E | 23.54° | 2025-09-18 12:05:33.620Z | 23.714° NE |
| 11 mins | 2025-09-18 13:41:33.620Z | 204.167° SW | 2025-09-18 13:46:33.620Z | 275.741° WNW | 37.375° | 2025-09-18 13:52:33.620Z | 347.468° N |
| 12 mins | 2025-09-19 00:50:33.620Z | 3.572° NNE | 2025-09-19 00:56:33.620Z | 132.073° SE | 44.389° | 2025-09-19 01:02:33.620Z | 178.411° S |
| 5 mins | 2025-09-19 02:39:33.620Z | 311.463° NW | 2025-09-19 02:41:33.620Z | 291.866° WNW | 15.068° | 2025-09-19 02:44:33.620Z | 262.399° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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