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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-29
1 61562U 24185L 25340.88809705 .00000280 00000-0 41522-3 0 9996
2 61562 88.9790 81.9139 0011520 73.9130 286.3289 13.51007926 67001Epoch: 2025-12-06T21:18Z
TLE epoch observation values (Epoch: 2025-12-06T21:18:51.585Z)
Latitude
0.00003°
Longitude
46.28959°
Altitude
1,069.102 km
Speed
7.319 km/s
True Right ascension
05h 27m 39s
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
13:18:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.179 km
Perigee altitude
1,057.028 km
Semi-major axis
7,443.741 km
Eccentricity
0.00115
Inclination
88.979°
RAAN
81.9139°
Arg. of periapsis
73.913°
True anomaly
286.20216°
Mean anomaly
286.3289°
Eccentric anomaly
286.26554°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.00041522
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-07 17:29:40.012Z | 46.245° ENE | 2025-12-07 17:32:40.012Z | 74.225° E | 13.638° | 2025-12-07 17:35:40.012Z | 102.267° ESE |
| 11 mins | 2025-12-07 19:14:40.012Z | 359.699° N | 2025-12-07 19:19:40.012Z | 338.536° N | 44.582° | 2025-12-07 19:25:40.012Z | 184.841° SSW |
| 11 mins | 2025-12-08 07:11:40.012Z | 173.784° S | 2025-12-08 07:16:40.012Z | 138.825° SSE | 44.548° | 2025-12-08 07:22:40.012Z | 0.96° NNE |
| 5 mins | 2025-12-08 09:02:40.012Z | 268.695° W | 2025-12-08 09:04:40.012Z | 288.661° WNW | 14.005° | 2025-12-08 09:07:40.012Z | 316.384° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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