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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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: 17 hours ago
TLE from 17 hours ago
0 QIANFAN-29
1 61562U 24185L 26235.54344977 .00000142 00000-0 20101-3 0 9995
2 61562 88.9764 55.0739 0011120 45.0475 315.1576 13.51087557102062Epoch: 2026-08-23T13:02Z
TLE epoch observation values (Epoch: 2026-08-23T13:02:34.060Z)
Latitude
-0.00001°
Longitude
-112.40601°
Altitude
1,065.345 km
Speed
7.322 km/s
True Right ascension
03h 40m 17s
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
20:47:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.588 km
Perigee altitude
1,057.034 km
Semi-major axis
7,443.448 km
Eccentricity
0.00111
Inclination
88.9764°
RAAN
55.0739°
Arg. of periapsis
45.0475°
True anomaly
315.06766°
Mean anomaly
315.1576°
Eccentric anomaly
315.11264°
Mean motion
3.37973 °/min
Orbital period
106.52 mins
BSTAR
0.00020101
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-08-24 12:15:46.965Z | 167.985° S | 2026-08-24 12:20:46.965Z | 82.869° E | 43.913° | 2026-08-24 12:26:46.965Z | 3.366° NNE |
| 6 mins | 2026-08-24 14:05:46.965Z | 261.559° W | 2026-08-24 14:07:46.965Z | 282.344° WNW | 16.042° | 2026-08-24 14:11:46.965Z | 320.913° NNW |
| 10 mins | 2026-08-24 23:25:46.965Z | 27.274° NE | 2026-08-24 23:29:46.965Z | 77.718° E | 30.159° | 2026-08-24 23:35:46.965Z | 146.902° SSE |
| 10 mins | 2026-08-25 01:11:46.965Z | 338.257° N | 2026-08-25 01:16:46.965Z | 275.535° WNW | 30.32° | 2026-08-25 01:21:46.965Z | 219.964° SW |
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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