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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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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-27
1 61560U 24185J 26251.83667071 .00000535 00000-0 21139-3 0 9994
2 61560 88.9827 45.2849 0009320 115.9905 244.2251 14.27596126108695Epoch: 2026-09-08T20:04Z
TLE epoch observation values (Epoch: 2026-09-08T20:04:48.349Z)
Latitude
0.00006°
Longitude
116.18608°
Altitude
805.756 km
Speed
7.449 km/s
True Right ascension
03h 01m 08s
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
00:18:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
803.405 km
Perigee altitude
790.031 km
Semi-major axis
7,174.855 km
Eccentricity
0.00093
Inclination
88.9827°
RAAN
45.2849°
Arg. of periapsis
115.9905°
True anomaly
244.12897°
Mean anomaly
244.2251°
Eccentric anomaly
244.17703°
Mean motion
3.57128 °/min
Orbital period
100.8 mins
BSTAR
0.00021139
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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
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-09 09:40:40.312Z | 119.334° SE | 2026-09-09 09:43:40.312Z | 80.42° E | 21.334° | 2026-09-09 09:47:40.312Z | 30.284° NE |
| 8 mins | 2026-09-09 11:20:40.312Z | 208.871° SW | 2026-09-09 11:24:40.312Z | 282.968° WNW | 42.685° | 2026-09-09 11:28:40.312Z | 341.957° N |
| 8 mins | 2026-09-09 21:54:40.312Z | 29.455° NE | 2026-09-09 21:57:40.312Z | 77.787° E | 34.321° | 2026-09-09 22:02:40.312Z | 149.46° SSE |
| 7 mins | 2026-09-09 23:35:40.312Z | 325.183° NNW | 2026-09-09 23:38:40.312Z | 280.056° WNW | 26.174° | 2026-09-09 23:42:40.312Z | 227.697° WSW |
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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