QIANFAN-45, 62246
Orbit data source: Space-Track
QIANFAN-45, 62246 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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62246 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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-45
1 62246U 24232K 25288.57208142 .00000134 00000-0 18874-3 0 9996
2 62246 89.0029 47.0722 0014089 8.7202 351.4191 13.50976505 91402Epoch: 2025-10-15T13:43Z
TLE epoch observation values (Epoch: 2025-10-15T13:43:47.834Z)
Latitude
-0.00006°
Longitude
176.77866°
Altitude
1,061.245 km
Speed
7.326 km/s
True Right ascension
03h 08m 17s
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
14:55:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.207 km
Perigee altitude
1,055.231 km
Semi-major axis
7,443.856 km
Eccentricity
0.00141
Inclination
89.0029°
RAAN
47.0722°
Arg. of periapsis
8.7202°
True anomaly
351.39497°
Mean anomaly
351.4191°
Eccentric anomaly
351.40704°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00018874
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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-45 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-10-15 21:26:42.154Z | 334.659° NNW | 2025-10-15 21:31:42.154Z | 277.241° WNW | 26.088° | 2025-10-15 21:36:42.154Z | 226.47° WSW |
| 10 mins | 2025-10-16 07:37:42.154Z | 139.629° SSE | 2025-10-16 07:42:42.154Z | 73.347° E | 31.661° | 2025-10-16 07:47:42.154Z | 17.568° NNE |
| 10 mins | 2025-10-16 09:24:42.154Z | 224.088° SW | 2025-10-16 09:28:42.154Z | 273.97° WNW | 28.535° | 2025-10-16 09:34:42.154Z | 340.046° N |
| 6 mins | 2025-10-16 18:48:42.154Z | 50.787° ENE | 2025-10-16 18:50:42.154Z | 71.751° E | 17.388° | 2025-10-16 18:54:42.154Z | 112.41° ESE |
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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