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 25256.23668890 .00000365 00000-0 14371-3 0 9993
2 61560 88.9742 87.5631 0006566 213.5648 146.5131 14.27160452 57252Epoch: 2025-09-13T05:40Z
TLE epoch observation values (Epoch: 2025-09-13T05:40:49.92Z)
Latitude
-0.00004°
Longitude
9.88216°
Altitude
808.235 km
Speed
7.447 km/s
True Right ascension
05h 50m 15s
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
15:41:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
802.891 km
Perigee altitude
793.467 km
Semi-major axis
7,176.316 km
Eccentricity
0.00066
Inclination
88.9742°
RAAN
87.5631°
Arg. of periapsis
213.5648°
True anomaly
146.55459°
Mean anomaly
146.5131°
Eccentric anomaly
146.53385°
Mean motion
3.57019 °/min
Orbital period
100.84 mins
BSTAR
0.00014371
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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 | 2025-09-14 00:46:09.716Z | 12.149° NNE | 2025-09-14 00:51:09.716Z | 107.667° ESE | 38.529° | 2025-09-14 00:55:09.716Z | 163.382° S |
| 5 mins | 2025-09-14 02:29:09.716Z | 309.754° NW | 2025-09-14 02:31:09.716Z | 283.558° WNW | 16.342° | 2025-09-14 02:34:09.716Z | 247.51° W |
| 6 mins | 2025-09-14 12:07:09.716Z | 113.347° SE | 2025-09-14 12:10:09.716Z | 72.025° E | 19.378° | 2025-09-14 12:13:09.716Z | 34.69° NE |
| 8 mins | 2025-09-14 13:47:09.716Z | 210.975° SW | 2025-09-14 13:50:09.716Z | 266.957° W | 35.142° | 2025-09-14 13:55:09.716Z | 345.034° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
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