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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-27
1 61560U 24185J 26135.26912579 .00000274 00000-0 10559-3 0 9992
2 61560 88.9835 58.9289 0008896 131.2648 228.9314 14.27510549 92062Epoch: 2026-05-15T06:27Z
TLE epoch observation values (Epoch: 2026-05-15T06:27:32.468Z)
Latitude
0°
Longitude
89.04075°
Altitude
807.327 km
Speed
7.447 km/s
True Right ascension
03h 55m 42s
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
09:21:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
803.388 km
Perigee altitude
790.622 km
Semi-major axis
7,175.142 km
Eccentricity
0.00089
Inclination
88.9835°
RAAN
58.9289°
Arg. of periapsis
131.2648°
True anomaly
228.8546°
Mean anomaly
228.9314°
Eccentric anomaly
228.89299°
Mean motion
3.57106 °/min
Orbital period
100.81 mins
BSTAR
0.00010559
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-16 06:35:01.265Z | 16.43° NNE | 2026-05-16 06:40:01.265Z | 90.396° ESE | 32.888° | 2026-05-16 06:44:01.265Z | 151.754° SSE |
| 6 mins | 2026-05-16 08:18:01.265Z | 317.401° NNW | 2026-05-16 08:20:01.265Z | 288.989° WNW | 20.656° | 2026-05-16 08:24:01.265Z | 235.602° WSW |
| 4 mins | 2026-05-16 17:58:01.265Z | 88.644° E | 2026-05-16 17:59:01.265Z | 75.669° E | 14.917° | 2026-05-16 18:02:01.265Z | 40.524° NE |
| 8 mins | 2026-05-16 19:36:01.265Z | 197.169° SSW | 2026-05-16 19:39:01.265Z | 251.876° W | 40.565° | 2026-05-16 19:44:01.265Z | 350.202° N |
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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