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: 17 hours ago
TLE from 17 hours ago
0 QIANFAN-29
1 61562U 24185L 25257.56604513 .00000154 00000-0 21993-3 0 9998
2 61562 88.9723 90.5336 0008837 317.8685 42.1786 13.50965173 55759Epoch: 2025-09-14T13:35Z
TLE epoch observation values (Epoch: 2025-09-14T13:35:06.299Z)
Latitude
-0.00001°
Longitude
-107.02586°
Altitude
1,066.788 km
Speed
7.321 km/s
True Right ascension
06h 02m 08s
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
23:16:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,072.339 km
Perigee altitude
1,059.183 km
Semi-major axis
7,443.898 km
Eccentricity
0.00088
Inclination
88.9723°
RAAN
90.5336°
Arg. of periapsis
317.8685°
True anomaly
42.24665°
Mean anomaly
42.1786°
Eccentric anomaly
42.21262°
Mean motion
3.37942 °/min
Orbital period
106.53 mins
BSTAR
0.00021993
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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 | 2025-09-15 12:47:53.193Z | 154.302° SSE | 2025-09-15 12:53:53.193Z | 72.299° E | 37.699° | 2025-09-15 12:58:53.193Z | 12.398° NNE |
| 8 mins | 2025-09-15 14:36:53.193Z | 239.545° WSW | 2025-09-15 14:39:53.193Z | 273.781° WNW | 22.784° | 2025-09-15 14:44:53.193Z | 329.031° NNW |
| 9 mins | 2025-09-15 23:58:53.193Z | 36.57° NE | 2025-09-16 00:02:53.193Z | 82.21° E | 22.666° | 2025-09-16 00:07:53.193Z | 132.062° SE |
| 11 mins | 2025-09-16 01:44:53.193Z | 345.397° N | 2025-09-16 01:49:53.193Z | 265.904° W | 38.121° | 2025-09-16 01:55:53.193Z | 203.156° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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