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 25261.25359388 .00000183 00000-0 26968-3 0 9996
2 61563 88.9740 89.6434 0005786 288.2952 71.7568 13.49944253 56532Epoch: 2025-09-18T06:05Z
TLE epoch observation values (Epoch: 2025-09-18T06:05:10.511Z)
Latitude
-0.00009°
Longitude
0.93176°
Altitude
1,074.068 km
Speed
7.316 km/s
True Right ascension
05h 58m 34s
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
11:34:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.826 km
Perigee altitude
1,065.207 km
Semi-major axis
7,447.653 km
Eccentricity
0.00058
Inclination
88.974°
RAAN
89.6434°
Arg. of periapsis
288.2952°
True anomaly
71.81978°
Mean anomaly
71.7568°
Eccentric anomaly
71.78829°
Mean motion
3.37687 °/min
Orbital period
106.61 mins
BSTAR
0.00026968
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-09-19 00:28:10.335Z | 11.221° NNE | 2025-09-19 00:34:10.335Z | 92.193° ESE | 39.53° | 2025-09-19 00:40:10.335Z | 163.972° S |
| 8 mins | 2025-09-19 02:16:10.335Z | 327.157° NNW | 2025-09-19 02:20:10.335Z | 284.254° WNW | 21.649° | 2025-09-19 02:24:10.335Z | 241.647° WSW |
| 10 mins | 2025-09-19 12:27:10.335Z | 147.916° SSE | 2025-09-19 12:31:10.335Z | 95.194° ESE | 36.713° | 2025-09-19 12:37:10.335Z | 12.653° NNE |
| 9 mins | 2025-09-19 14:14:10.335Z | 231.642° WSW | 2025-09-19 14:18:10.335Z | 275.36° WNW | 23.811° | 2025-09-19 14:23:10.335Z | 330.537° NNW |
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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