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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-46
1 62247U 24232L 25339.92343416 .00000177 00000-0 25524-3 0 9994
2 62247 89.0034 41.9758 0013747 211.0312 149.0029 13.50979650 98291Epoch: 2025-12-05T22:09Z
TLE epoch observation values (Epoch: 2025-12-05T22:09:44.711Z)
Latitude
0.00004°
Longitude
-5.41906°
Altitude
1,080.39 km
Speed
7.308 km/s
True Right ascension
02h 47m 54s
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
05:14:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.94 km
Perigee altitude
1,055.474 km
Semi-major axis
7,443.844 km
Eccentricity
0.00137
Inclination
89.0034°
RAAN
41.9758°
Arg. of periapsis
211.0312°
True anomaly
149.08391°
Mean anomaly
149.0029°
Eccentric anomaly
149.04342°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00025524
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-06 14:48:11.073Z | 53.729° ENE | 2025-12-06 14:50:11.073Z | 71.926° E | 11.788° | 2025-12-06 14:52:11.073Z | 90.33° ESE |
| 12 mins | 2025-12-06 16:32:11.073Z | 2.553° NNE | 2025-12-06 16:38:11.073Z | 149.714° SSE | 44.536° | 2025-12-06 16:44:11.073Z | 180.207° SSW |
| 5 mins | 2025-12-06 18:21:11.073Z | 310.569° NW | 2025-12-06 18:23:11.073Z | 291.2° WNW | 14.199° | 2025-12-06 18:26:11.073Z | 262.479° W |
| 12 mins | 2025-12-07 04:29:11.073Z | 168.771° S | 2025-12-07 04:35:11.073Z | 50.254° ENE | 43.467° | 2025-12-07 04:41:11.073Z | 2.923° NNE |
| 6 mins | 2025-12-07 06:19:11.073Z | 256.485° W | 2025-12-07 06:22:11.073Z | 287.024° WNW | 16.27° | 2025-12-07 06:25:11.073Z | 316.252° 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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