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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-27
1 61560U 24185J 25361.47061426 .00000678 00000-0 27097-3 0 9994
2 61560 88.9798 75.2196 0006155 228.5314 131.5352 14.27351085 72264Epoch: 2025-12-27T11:17Z
TLE epoch observation values (Epoch: 2025-12-27T11:17:41.072Z)
Latitude
-0.00002°
Longitude
169.60198°
Altitude
806.594 km
Speed
7.448 km/s
True Right ascension
05h 00m 52s
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
17:27:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
801.956 km
Perigee altitude
793.123 km
Semi-major axis
7,175.677 km
Eccentricity
0.00062
Inclination
88.9798°
RAAN
75.2196°
Arg. of periapsis
228.5314°
True anomaly
131.58797°
Mean anomaly
131.5352°
Eccentric anomaly
131.56159°
Mean motion
3.57066 °/min
Orbital period
100.82 mins
BSTAR
0.00027097
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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 | 2025-12-27 18:36:51.088Z | 326.496° NNW | 2025-12-27 18:39:51.088Z | 289.913° WNW | 19.286° | 2025-12-27 18:43:51.088Z | 238.377° WSW |
| 5 mins | 2025-12-28 04:16:51.088Z | 102.621° ESE | 2025-12-28 04:18:51.088Z | 76.991° E | 16.334° | 2025-12-28 04:21:51.088Z | 40.351° NE |
| 8 mins | 2025-12-28 05:55:51.088Z | 200.607° SSW | 2025-12-28 05:58:51.088Z | 250.991° W | 38.683° | 2025-12-28 06:03:51.088Z | 347.91° N |
| 7 mins | 2025-12-28 16:29:51.088Z | 35.135° NE | 2025-12-28 16:32:51.088Z | 80.195° E | 24.849° | 2025-12-28 16:36:51.088Z | 136.753° SSE |
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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