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: 14 hours ago
TLE from 14 hours ago
0 QIANFAN-30
1 61563U 24185M 26235.56223986 .00000144 00000-0 20808-3 0 9990
2 61563 88.9784 54.6946 0008574 34.9598 325.2114 13.50069516102314Epoch: 2026-08-23T13:29Z
TLE epoch observation values (Epoch: 2026-08-23T13:29:37.523Z)
Latitude
-0.00006°
Longitude
-119.56826°
Altitude
1,069.709 km
Speed
7.32 km/s
True Right ascension
03h 38m 46s
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
18:59:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.441 km
Perigee altitude
1,062.67 km
Semi-major axis
7,447.192 km
Eccentricity
0.00086
Inclination
88.9784°
RAAN
54.6946°
Arg. of periapsis
34.9598°
True anomaly
325.15529°
Mean anomaly
325.2114°
Eccentric anomaly
325.18335°
Mean motion
3.37718 °/min
Orbital period
106.6 mins
BSTAR
0.00020808
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-24 10:59:15.064Z | 110.382° ESE | 2026-08-24 11:03:15.064Z | 69.468° E | 18.048° | 2026-08-24 11:06:15.064Z | 39.093° NE |
| 11 mins | 2026-08-24 12:44:15.064Z | 192.478° SSW | 2026-08-24 12:49:15.064Z | 294.193° NW | 42.263° | 2026-08-24 12:55:15.064Z | 353.588° N |
| 11 mins | 2026-08-24 23:54:15.064Z | 13.159° NNE | 2026-08-24 23:59:15.064Z | 105.413° ESE | 40.876° | 2026-08-25 00:05:15.064Z | 167.912° S |
| 8 mins | 2026-08-25 01:41:15.064Z | 323.532° NNW | 2026-08-25 01:45:15.064Z | 280.573° WNW | 19.845° | 2026-08-25 01:49:15.064Z | 241.681° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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