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). Payloads include a variety of satellites, spacecraft, and rockets 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)
QIANFAN-32 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 11 hours ago |
| Origin | |
| Manufacturer | GESIH/SECM |
| Mission | Operational Commercial Communications |
| Bus & Motor | QIANFAN, Unknown motor |
| Mass | 300 kg wet, ~300 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 1 Pan, 10 m |
| Radar Cross Section | 13.200 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 11 hours ago
0 QIANFAN-32
1 61565U 24185P 25035.79916930 .00000191 00000-0 96847-4 0 9991
2 61565 88.9874 113.4279 0007185 209.3869 150.6913 14.11845050 25779Epoch: 2025-02-04T19:10Z
Definitive object data (Epoch: 2025-02-04T19:10:48.227Z)
| Latitude | -0.00007° |
| Longitude | 50.52768° |
| Altitude | 860.639 km |
| Speed | 7.42 km/s |
| True Right ascension | 07h 33m 42s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 39.55313° |
| Longitude | -130.35564° |
| Altitude | 856.768 km |
| Speed | 7.429 km/s |
| Apparent Right ascension | 19h 46m 29s |
| Apparent Declination | 2° 49' 06" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 08:05:06 |
| Azimuth | 6.828° NNE |
| Elevation | -47.053° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 855.221 km |
| Perigee altitude | 844.834 km |
| Semi-major axis | 7,228.165 km |
| Eccentricity | 0.0007185 |
| Inclination | 88.9874° |
| RAAN | 113.4279° |
| Arg. of periapsis | 209.3869° |
| True anomaly | 150.73157° |
| Mean anomaly | 150.6913° |
| Eccentric anomaly | 150.71144° |
| Mean motion | 3.53184 °/min |
| BSTAR | 0.000096847 |
| Orbital period | 101.93 mins |
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Other satellites on launch #185 in the year 2024 (2024-10-15 UTC)
QIANFAN-32 Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-02-05 16:11:59.474Z | 41.852° NE | 2025-02-05 16:14:59.474Z | 80.904° E | 19.733° | 2025-02-05 16:18:59.474Z | 127.907° SE |
| 9 mins | 2025-02-05 17:52:59.474Z | 344.39° N | 2025-02-05 17:56:59.474Z | 282.049° WNW | 36.129° | 2025-02-05 18:01:59.474Z | 206.227° SW |
| 9 mins | 2025-02-06 05:18:59.474Z | 171.329° S | 2025-02-06 05:22:59.474Z | 124.543° SE | 44.079° | 2025-02-06 05:27:59.474Z | 2.522° NNE |
Authenticating...
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