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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-29
1 61562U 24185L 26072.53865725 .00000227 00000-0 33300-3 0 9991
2 61562 88.9723 71.9073 0011043 138.8060 221.3927 13.51047049 80054Epoch: 2026-03-13T12:55Z
TLE epoch observation values (Epoch: 2026-03-13T12:55:39.986Z)
Latitude
0.00003°
Longitude
66.81794°
Altitude
1,077.536 km
Speed
7.31 km/s
True Right ascension
04h 47m 37s
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
01:17:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,073.68 km
Perigee altitude
1,057.24 km
Semi-major axis
7,443.597 km
Eccentricity
0.0011
Inclination
88.9723°
RAAN
71.9073°
Arg. of periapsis
138.806°
True anomaly
221.30911°
Mean anomaly
221.3927°
Eccentric anomaly
221.3509°
Mean motion
3.37963 °/min
Orbital period
106.52 mins
BSTAR
0.000333
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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 | 2026-03-13 23:42:08.368Z | 150.665° SSE | 2026-03-13 23:47:08.368Z | 92.755° ESE | 36.135° | 2026-03-13 23:53:08.368Z | 12.977° NNE |
| 9 mins | 2026-03-14 01:30:08.368Z | 231.902° WSW | 2026-03-14 01:34:08.368Z | 277.583° WNW | 24.409° | 2026-03-14 01:39:08.368Z | 332.132° NNW |
| 8 mins | 2026-03-14 10:53:08.368Z | 40.941° NE | 2026-03-14 10:56:08.368Z | 74.145° E | 20.902° | 2026-03-14 11:01:08.368Z | 126.409° SE |
| 11 mins | 2026-03-14 12:38:08.368Z | 349.372° N | 2026-03-14 12:43:08.368Z | 285.898° WNW | 39.571° | 2026-03-14 12:49:08.368Z | 201.87° SSW |
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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