QIANFAN-46, 62247
Orbit data source: Space-Track
QIANFAN-46, 62247 is a Chinese payload satellite in LEO that was launched on Thu, 05 Dec 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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62247 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
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: 16 hours ago
TLE from 16 hours ago
0 QIANFAN-46
1 62247U 24232L 25287.93016257 .00000154 00000-0 21971-3 0 9994
2 62247 89.0024 47.2083 0014418 16.0652 344.0954 13.50977050 91273Epoch: 2025-10-14T22:19Z
TLE epoch observation values (Epoch: 2025-10-14T22:19:26.046Z)
Latitude
0.00006°
Longitude
48.63825°
Altitude
1,061.292 km
Speed
7.326 km/s
True Right ascension
03h 08m 49s
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
09:05:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.45 km
Perigee altitude
1,054.984 km
Semi-major axis
7,443.854 km
Eccentricity
0.00144
Inclination
89.0024°
RAAN
47.2083°
Arg. of periapsis
16.0652°
True anomaly
344.05005°
Mean anomaly
344.0954°
Eccentric anomaly
344.07273°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00021971
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Other satellites on launch #232 in the year 2024 (2024-12-05 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-46 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 | 2025-10-15 20:15:28.917Z | 3.909° NNE | 2025-10-15 20:20:28.917Z | 61.421° ENE | 44.58° | 2025-10-15 20:26:28.917Z | 178.25° S |
| 5 mins | 2025-10-15 22:04:28.917Z | 307.054° NW | 2025-10-15 22:06:28.917Z | 286.89° WNW | 15.015° | 2025-10-15 22:09:28.917Z | 258.525° W |
| 11 mins | 2025-10-16 08:12:28.917Z | 166.612° S | 2025-10-16 08:17:28.917Z | 97.027° ESE | 43.448° | 2025-10-16 08:23:28.917Z | 4.29° NNE |
| 6 mins | 2025-10-16 10:02:28.917Z | 259.142° W | 2025-10-16 10:04:28.917Z | 280.088° WNW | 16.617° | 2025-10-16 10:08:28.917Z | 319.853° 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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