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 26035.82012727 .00000152 00000-0 22000-3 0 9991
2 61563 88.9752 75.2666 0006083 228.2220 131.8412 13.50008617 75361Epoch: 2026-02-04T19:40Z
TLE epoch observation values (Epoch: 2026-02-04T19:40:58.996Z)
Latitude
0.00007°
Longitude
5.03956°
Altitude
1,078.204 km
Speed
7.311 km/s
True Right ascension
05h 01m 03s
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
03:05:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.81 km
Perigee altitude
1,064.749 km
Semi-major axis
7,447.416 km
Eccentricity
0.00061
Inclination
88.9752°
RAAN
75.2666°
Arg. of periapsis
228.222°
True anomaly
131.8931°
Mean anomaly
131.8412°
Eccentric anomaly
131.86715°
Mean motion
3.37703 °/min
Orbital period
106.6 mins
BSTAR
0.00022
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-05 01:12:16.108Z | 87.4° E | 2026-02-05 01:14:16.108Z | 68.971° E | 12.276° | 2026-02-05 01:16:16.108Z | 50.685° ENE |
| 12 mins | 2026-02-05 02:54:16.108Z | 174.366° S | 2026-02-05 02:59:16.108Z | 150.937° SSE | 44.392° | 2026-02-05 03:06:16.108Z | 0.529° NNE |
| 5 mins | 2026-02-05 04:45:16.108Z | 267.017° W | 2026-02-05 04:47:16.108Z | 286.604° WNW | 14.085° | 2026-02-05 04:50:16.108Z | 314.517° NW |
| 10 mins | 2026-02-05 14:05:16.108Z | 23.204° NE | 2026-02-05 14:09:16.108Z | 74.378° E | 33.255° | 2026-02-05 14:15:16.108Z | 151.401° SSE |
| 9 mins | 2026-02-05 15:52:16.108Z | 329.968° NNW | 2026-02-05 15:56:16.108Z | 279.379° WNW | 27.238° | 2026-02-05 16:01:16.108Z | 225.544° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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