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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-30
1 61563U 24185M 25310.91432443 .00000220 00000-0 32762-3 0 9999
2 61563 88.9783 84.5175 0008909 133.0306 227.1592 13.49968493 63236Epoch: 2025-11-06T21:56Z
TLE epoch observation values (Epoch: 2025-11-06T21:56:37.630Z)
Latitude
-0.00006°
Longitude
68.9949°
Altitude
1,079.844 km
Speed
7.31 km/s
True Right ascension
05h 38m 04s
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
00:33:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.062 km
Perigee altitude
1,062.792 km
Semi-major axis
7,447.564 km
Eccentricity
0.00089
Inclination
88.9783°
RAAN
84.5175°
Arg. of periapsis
133.0306°
True anomaly
227.0844°
Mean anomaly
227.1592°
Eccentric anomaly
227.12179°
Mean motion
3.37693 °/min
Orbital period
106.61 mins
BSTAR
0.00032762
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-07 08:43:38.920Z | 145.552° SSE | 2025-11-07 08:48:38.920Z | 90.369° ESE | 33.111° | 2025-11-07 08:54:38.920Z | 15.61° NNE |
| 9 mins | 2025-11-07 10:31:38.920Z | 227.227° WSW | 2025-11-07 10:35:38.920Z | 276.311° WNW | 27.365° | 2025-11-07 10:40:38.920Z | 334.202° NNW |
| 7 mins | 2025-11-07 19:55:38.920Z | 47.274° ENE | 2025-11-07 19:58:38.920Z | 80.192° E | 18.609° | 2025-11-07 20:02:38.920Z | 119.621° SE |
| 11 mins | 2025-11-07 21:40:38.920Z | 351.507° N | 2025-11-07 21:45:38.920Z | 270.085° WNW | 42.014° | 2025-11-07 21:51:38.920Z | 196.167° SSW |
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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