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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-27
1 61560U 24185J 26071.90038575 .00000656 00000-0 26162-3 0 9998
2 61560 88.9755 66.3511 0007834 11.5491 348.5881 14.27452418 83025Epoch: 2026-03-12T21:36Z
TLE epoch observation values (Epoch: 2026-03-12T21:36:33.328Z)
Latitude
-0.00009°
Longitude
-68.33141°
Altitude
797.809 km
Speed
7.457 km/s
True Right ascension
04h 25m 24s
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
09:02:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
802.821 km
Perigee altitude
791.579 km
Semi-major axis
7,175.337 km
Eccentricity
0.00078
Inclination
88.9755°
RAAN
66.3511°
Arg. of periapsis
11.5491°
True anomaly
348.57032°
Mean anomaly
348.5881°
Eccentric anomaly
348.57921°
Mean motion
3.57092 °/min
Orbital period
100.81 mins
BSTAR
0.00026162
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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 | 2026-03-13 11:38:56.076Z | 8.416° NNE | 2026-03-13 11:42:56.076Z | 62.253° ENE | 41.945° | 2026-03-13 11:47:56.076Z | 170.828° S |
| 4 mins | 2026-03-13 13:21:56.076Z | 305.568° NW | 2026-03-13 13:23:56.076Z | 281.146° WNW | 13.638° | 2026-03-13 13:25:56.076Z | 258.195° W |
| 6 mins | 2026-03-13 22:59:56.076Z | 114.1° SE | 2026-03-13 23:01:56.076Z | 83.658° E | 22.38° | 2026-03-13 23:05:56.076Z | 29.195° NE |
| 7 mins | 2026-03-14 00:39:56.076Z | 220.889° SW | 2026-03-14 00:42:56.076Z | 276.939° WNW | 30.973° | 2026-03-14 00:46:56.076Z | 337.844° 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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