QIANFAN-27, 61560
Orbit data source: Space-Track
QIANFAN-27, 61560 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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61560 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH/SECM
Mission
Partially 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: 17 hours ago
TLE from 17 hours ago
0 QIANFAN-27
1 61560U 24185J 25300.89812434 .00000869 00000-0 34965-3 0 9990
2 61560 88.9771 82.3114 0010032 83.1918 277.0417 14.27244556 63620Epoch: 2025-10-27T21:33Z
TLE epoch observation values (Epoch: 2025-10-27T21:33:17.942Z)
Latitude
-0.00008°
Longitude
82.49327°
Altitude
803.143 km
Speed
7.452 km/s
True Right ascension
05h 29m 14s
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
09:38:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
805.096 km
Perigee altitude
790.698 km
Semi-major axis
7,176.034 km
Eccentricity
0.001
Inclination
88.9771°
RAAN
82.3114°
Arg. of periapsis
83.1918°
True anomaly
276.92759°
Mean anomaly
277.0417°
Eccentric anomaly
276.98465°
Mean motion
3.5704 °/min
Orbital period
100.83 mins
BSTAR
0.00034965
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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-27 Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-28 21:41:25.841Z | 6.006° NNE | 2025-10-28 21:45:25.841Z | 48.161° ENE | 42.809° | 2025-10-28 21:50:25.841Z | 174.213° S |
| 6 mins | 2025-10-29 09:02:25.841Z | 119.012° SE | 2025-10-29 09:04:25.841Z | 88.17° E | 24.007° | 2025-10-29 09:08:25.841Z | 29.2° NE |
| 7 mins | 2025-10-29 10:42:25.841Z | 222.093° SW | 2025-10-29 10:45:25.841Z | 271.281° WNW | 28.83° | 2025-10-29 10:49:25.841Z | 334.236° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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