QIANFAN-30, 61563
Orbit data source: Space-Track
QIANFAN-30, 61563 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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61563 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
GESIH/SECM
Mission
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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-30
1 61563U 24185M 25306.46712910 .00000199 00000-0 29410-3 0 9995
2 61563 88.9777 84.9755 0008658 143.7103 216.4636 13.49966362 62637Epoch: 2025-11-02T11:12Z
TLE epoch observation values (Epoch: 2025-11-02T11:12:39.954Z)
Latitude
-0.00004°
Longitude
-125.17342°
Altitude
1,080.525 km
Speed
7.309 km/s
True Right ascension
05h 39m 54s
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
20:16:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.883 km
Perigee altitude
1,062.987 km
Semi-major axis
7,447.572 km
Eccentricity
0.00087
Inclination
88.9777°
RAAN
84.9755°
Arg. of periapsis
143.7103°
True anomaly
216.40469°
Mean anomaly
216.4636°
Eccentric anomaly
216.43414°
Mean motion
3.37692 °/min
Orbital period
106.61 mins
BSTAR
0.0002941
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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-30 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-03 08:40:27.894Z | 132.516° SE | 2025-11-03 08:45:27.894Z | 81.701° E | 25.552° | 2025-11-03 08:50:27.894Z | 25.42° NE |
| 10 mins | 2025-11-03 10:27:27.894Z | 209.944° SW | 2025-11-03 10:32:27.894Z | 284.661° WNW | 35.073° | 2025-11-03 10:37:27.894Z | 343.191° N |
| 12 mins | 2025-11-03 21:36:27.894Z | 1.192° NNE | 2025-11-03 21:42:27.894Z | 176.134° S | 44.613° | 2025-11-03 21:48:27.894Z | 182.345° SSW |
| 4 mins | 2025-11-03 23:26:27.894Z | 301.41° NW | 2025-11-03 23:27:27.894Z | 291.679° WNW | 13.289° | 2025-11-03 23:30:27.894Z | 263.722° W |
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
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