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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-30
1 61563U 24185M 25312.47084081 .00000260 00000-0 38963-3 0 9996
2 61563 88.9784 84.3574 0008974 129.3784 230.8163 13.49969469 63440Epoch: 2025-11-08T11:18Z
TLE epoch observation values (Epoch: 2025-11-08T11:18:00.645Z)
Latitude
-0.00003°
Longitude
-133.04527°
Altitude
1,079.551 km
Speed
7.31 km/s
True Right ascension
05h 37m 25s
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
16:07:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.107 km
Perigee altitude
1,062.74 km
Semi-major axis
7,447.561 km
Eccentricity
0.0009
Inclination
88.9784°
RAAN
84.3574°
Arg. of periapsis
129.3784°
True anomaly
230.73665°
Mean anomaly
230.8163°
Eccentric anomaly
230.77647°
Mean motion
3.37693 °/min
Orbital period
106.61 mins
BSTAR
0.00038963
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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 | 2025-11-08 20:47:30.837Z | 11.707° NNE | 2025-11-08 20:53:30.837Z | 101.065° ESE | 39.399° | 2025-11-08 20:59:30.837Z | 164.945° S |
| 8 mins | 2025-11-08 22:35:30.837Z | 325.221° NNW | 2025-11-08 22:39:30.837Z | 280.991° WNW | 21.242° | 2025-11-08 22:43:30.837Z | 240.037° WSW |
| 11 mins | 2025-11-09 08:45:30.837Z | 151.694° SSE | 2025-11-09 08:50:30.837Z | 89.905° E | 37.142° | 2025-11-09 08:56:30.837Z | 11.8° NNE |
| 9 mins | 2025-11-09 10:33:30.837Z | 233.365° WSW | 2025-11-09 10:37:30.837Z | 278.229° WNW | 23.618° | 2025-11-09 10:42:30.837Z | 331.665° 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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