QIANFAN-29, 61562
Orbit data source: Space-Track
QIANFAN-29, 61562 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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61562 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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-29
1 61562U 24185L 25311.26278641 .00000249 00000-0 36640-3 0 9995
2 61562 88.9763 84.9700 0011175 146.9282 213.2570 13.50992198 63004Epoch: 2025-11-07T06:18Z
TLE epoch observation values (Epoch: 2025-11-07T06:18:24.745Z)
Latitude
-0.00004°
Longitude
-56.34237°
Altitude
1,078.526 km
Speed
7.309 km/s
True Right ascension
05h 39m 52s
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
10:43:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.98 km
Perigee altitude
1,057.343 km
Semi-major axis
7,443.798 km
Eccentricity
0.00112
Inclination
88.9763°
RAAN
84.97°
Arg. of periapsis
146.9282°
True anomaly
213.18686°
Mean anomaly
213.257°
Eccentric anomaly
213.22192°
Mean motion
3.37949 °/min
Orbital period
106.52 mins
BSTAR
0.0003664
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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-29 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 | 2025-11-07 21:06:39.155Z | 5.302° NNE | 2025-11-07 21:12:39.155Z | 61.627° ENE | 43.032° | 2025-11-07 21:18:39.155Z | 172.408° S |
| 6 mins | 2025-11-07 22:56:39.155Z | 310.649° NW | 2025-11-07 22:58:39.155Z | 289.476° WNW | 16.982° | 2025-11-07 23:02:39.155Z | 250.131° W |
| 11 mins | 2025-11-08 09:04:39.155Z | 161.281° S | 2025-11-08 09:09:39.155Z | 103.365° ESE | 41.197° | 2025-11-08 09:15:39.155Z | 7.706° NNE |
| 8 mins | 2025-11-08 10:53:39.155Z | 245.602° WSW | 2025-11-08 10:56:39.155Z | 276.891° WNW | 19.196° | 2025-11-08 11:01:39.155Z | 327.216° 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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