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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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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-46
1 62247U 24232L 26305.16833497 .00000082 00000-0 10859-3 0 9997
2 62247 89.0160 8.8777 0013505 352.3518 7.7425 13.51279500142886Epoch: 2026-11-01T04:02Z
TLE epoch observation values (Epoch: 2026-11-01T04:02:24.141Z)
Latitude
-0.00004°
Longitude
-92.18647°
Altitude
1,060.543 km
Speed
7.327 km/s
True Right ascension
00h 35m 30s
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
06:20:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.657 km
Perigee altitude
1,054.554 km
Semi-major axis
7,442.742 km
Eccentricity
0.00135
Inclination
89.016°
RAAN
8.8777°
Arg. of periapsis
352.3518°
True anomaly
7.76338°
Mean anomaly
7.7425°
Eccentric anomaly
7.75294°
Mean motion
3.38021 °/min
Orbital period
106.5 mins
BSTAR
0.00010859
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-11-01 15:18:56.939Z | 35.159° NE | 2026-11-01 15:22:56.939Z | 74.835° E | 20.558° | 2026-11-01 15:27:56.939Z | 123.937° SE |
| 11 mins | 2026-11-01 17:04:56.939Z | 351.687° N | 2026-11-01 17:09:56.939Z | 286.361° WNW | 62.488° | 2026-11-01 17:15:56.939Z | 197.904° SSW |
| 6 mins | 2026-11-02 03:18:56.939Z | 96.582° ESE | 2026-11-02 03:20:56.939Z | 75.497° E | 17.807° | 2026-11-02 03:24:56.939Z | 36.237° NE |
| 11 mins | 2026-11-02 05:01:56.939Z | 188.412° SSW | 2026-11-02 05:06:56.939Z | 271.241° WNW | 71.656° | 2026-11-02 05:12:56.939Z | 354.102° N |
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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