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: 5 hours ago
TLE from 5 hours ago
0 QIANFAN-30
1 61563U 24185M 25290.16068885 .00000272 00000-0 40978-3 0 9993
2 61563 88.9755 86.6564 0007264 186.3120 173.7940 13.49959203 60439Epoch: 2025-10-17T03:51Z
TLE epoch observation values (Epoch: 2025-10-17T03:51:23.516Z)
Latitude
-0.00006°
Longitude
2.89837°
Altitude
1,080.742 km
Speed
7.309 km/s
True Right ascension
05h 46m 37s
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
03:46:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.871 km
Perigee altitude
1,064.051 km
Semi-major axis
7,447.598 km
Eccentricity
0.00073
Inclination
88.9755°
RAAN
86.6564°
Arg. of periapsis
186.312°
True anomaly
173.80299°
Mean anomaly
173.794°
Eccentric anomaly
173.7985°
Mean motion
3.3769 °/min
Orbital period
106.61 mins
BSTAR
0.00040978
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-17 09:21:26.446Z | 99.567° ESE | 2025-10-17 09:24:26.446Z | 71.297° E | 14.525° | 2025-10-17 09:27:26.446Z | 43.017° NE |
| 11 mins | 2025-10-17 11:05:26.446Z | 181.23° SSW | 2025-10-17 11:10:26.446Z | 318.091° NNW | 44.624° | 2025-10-17 11:16:26.446Z | 357.697° N |
| 11 mins | 2025-10-17 22:15:26.446Z | 18.211° NNE | 2025-10-17 22:20:26.446Z | 92.633° ESE | 36.629° | 2025-10-17 22:26:26.446Z | 159.326° S |
| 9 mins | 2025-10-18 00:02:26.446Z | 329.028° NNW | 2025-10-18 00:06:26.446Z | 283.401° WNW | 24.168° | 2025-10-18 00:11:26.446Z | 231.161° WSW |
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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