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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-30
1 61563U 24185M 25342.26676159 .00000220 00000-0 32707-3 0 9995
2 61563 88.9810 81.2955 0008765 59.9669 300.2350 13.49987145 67464Epoch: 2025-12-08T06:24Z
TLE epoch observation values (Epoch: 2025-12-08T06:24:08.201Z)
Latitude
-0.00002°
Longitude
-92.00693°
Altitude
1,071.973 km
Speed
7.318 km/s
True Right ascension
05h 25m 10s
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
17:01:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.886 km
Perigee altitude
1,062.831 km
Semi-major axis
7,447.495 km
Eccentricity
0.00088
Inclination
88.981°
RAAN
81.2955°
Arg. of periapsis
59.9669°
True anomaly
300.14818°
Mean anomaly
300.235°
Eccentric anomaly
300.19159°
Mean motion
3.37697 °/min
Orbital period
106.6 mins
BSTAR
0.00032707
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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 | 2025-12-08 19:26:48.620Z | 352.812° N | 2025-12-08 19:32:48.620Z | 266.424° W | 41.532° | 2025-12-08 19:38:48.620Z | 197.08° SSW |
| 6 mins | 2025-12-09 05:41:48.620Z | 99.021° ESE | 2025-12-09 05:43:48.620Z | 78.267° E | 17.084° | 2025-12-09 05:47:48.620Z | 37.971° NE |
| 11 mins | 2025-12-09 07:24:48.620Z | 188.293° SSW | 2025-12-09 07:29:48.620Z | 248.512° W | 43.126° | 2025-12-09 07:35:48.620Z | 353.358° N |
| 11 mins | 2025-12-09 18:34:48.620Z | 11.846° NNE | 2025-12-09 18:39:48.620Z | 73.404° E | 39.964° | 2025-12-09 18:45:48.620Z | 164.033° S |
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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