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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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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-30
1 61563U 24185M 26304.19164194 .00000135 00000-0 19401-3 0 9998
2 61563 88.9886 47.6580 0008192 171.9782 188.1501 13.50085890111573Epoch: 2026-10-31T04:35Z
TLE epoch observation values (Epoch: 2026-10-31T04:35:57.863Z)
Latitude
-0.00004°
Longitude
-60.834°
Altitude
1,080.937 km
Speed
7.309 km/s
True Right ascension
03h 10m 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
06:34:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.096 km
Perigee altitude
1,062.894 km
Semi-major axis
7,447.132 km
Eccentricity
0.00082
Inclination
88.9886°
RAAN
47.658°
Arg. of periapsis
171.9782°
True anomaly
188.13681°
Mean anomaly
188.1501°
Eccentric anomaly
188.14345°
Mean motion
3.37722 °/min
Orbital period
106.6 mins
BSTAR
0.00019401
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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 | 2026-10-31 17:40:33.503Z | 44.034° NE | 2026-10-31 17:43:33.503Z | 71.656° E | 14.472° | 2026-10-31 17:46:33.503Z | 100.417° ESE |
| 11 mins | 2026-10-31 19:26:33.503Z | 358.932° N | 2026-10-31 19:31:33.503Z | 222.188° SW | 81.159° | 2026-10-31 19:37:33.503Z | 185.576° SSW |
| 4 mins | 2026-11-01 05:41:33.503Z | 84.059° E | 2026-11-01 05:43:33.503Z | 65.234° ENE | 12.808° | 2026-11-01 05:45:33.503Z | 47.274° ENE |
| 11 mins | 2026-11-01 07:23:33.503Z | 174.983° S | 2026-11-01 07:28:33.503Z | 106.089° ESE | 85.836° | 2026-11-01 07:34:33.503Z | 0.226° NNE |
| 4 mins | 2026-11-01 09:14:33.503Z | 270.958° WNW | 2026-11-01 09:16:33.503Z | 290.611° WNW | 14.185° | 2026-11-01 09:18:33.503Z | 309.345° NW |
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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