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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-27
1 61560U 24185J 26162.88708356 .00000348 00000-0 13550-3 0 9992
2 61560 88.9829 55.7044 0009616 61.8953 298.3212 14.27533343 96000Epoch: 2026-06-11T21:17Z
TLE epoch observation values (Epoch: 2026-06-11T21:17:24.019Z)
Latitude
-0.00004°
Longitude
-163.87012°
Altitude
799.781 km
Speed
7.455 km/s
True Right ascension
03h 42m 49s
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
16:57:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
803.828 km
Perigee altitude
790.029 km
Semi-major axis
7,175.065 km
Eccentricity
0.00096
Inclination
88.9829°
RAAN
55.7044°
Arg. of periapsis
61.8953°
True anomaly
298.22414°
Mean anomaly
298.3212°
Eccentric anomaly
298.27268°
Mean motion
3.57112 °/min
Orbital period
100.81 mins
BSTAR
0.0001355
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-12 15:57:30.528Z | 99.466° ESE | 2026-06-12 15:59:30.528Z | 74.812° E | 14.516° | 2026-06-12 16:01:30.528Z | 50.115° ENE |
| 8 mins | 2026-06-12 17:36:30.528Z | 196.584° SSW | 2026-06-12 17:39:30.528Z | 254.471° W | 40.994° | 2026-06-12 17:44:30.528Z | 350.813° N |
| 7 mins | 2026-06-13 04:10:30.528Z | 40.419° NE | 2026-06-13 04:13:30.528Z | 85.974° E | 22.677° | 2026-06-13 04:17:30.528Z | 136.001° SSE |
| 8 mins | 2026-06-13 05:50:30.528Z | 337.526° N | 2026-06-13 05:54:30.528Z | 270.602° WNW | 30.601° | 2026-06-13 05:58:30.528Z | 215.494° SW |
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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