QIANFAN-40, 62241
Orbit data source: Space-Track
QIANFAN-40, 62241 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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62241 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: 6 hours ago
TLE from 6 hours ago
0 QIANFAN-40
1 62241U 24232E 25288.61319542 .00000179 00000-0 25906-3 0 9996
2 62241 89.0052 46.6645 0013629 18.9554 341.2102 13.50979088 91749Epoch: 2025-10-15T14:43Z
TLE epoch observation values (Epoch: 2025-10-15T14:43:00.084Z)
Latitude
0.00002°
Longitude
161.52939°
Altitude
1,062.003 km
Speed
7.326 km/s
True Right ascension
03h 06m 39s
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
14:55:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.855 km
Perigee altitude
1,055.564 km
Semi-major axis
7,443.846 km
Eccentricity
0.00136
Inclination
89.0052°
RAAN
46.6645°
Arg. of periapsis
18.9554°
True anomaly
341.15981°
Mean anomaly
341.2102°
Eccentric anomaly
341.18502°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00025906
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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-40 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-15 20:38:40.649Z | 353.49° N | 2025-10-15 20:44:40.649Z | 256.055° W | 42.065° | 2025-10-15 20:50:40.649Z | 195.125° SSW |
| 6 mins | 2025-10-16 06:52:40.649Z | 101.333° ESE | 2025-10-16 06:55:40.649Z | 70.965° E | 16.208° | 2025-10-16 06:58:40.649Z | 41.328° NE |
| 11 mins | 2025-10-16 08:36:40.649Z | 187.198° SSW | 2025-10-16 08:41:40.649Z | 301.177° NW | 43.593° | 2025-10-16 08:47:40.649Z | 355.476° N |
| 11 mins | 2025-10-16 19:45:40.649Z | 14.077° NNE | 2025-10-16 19:50:40.649Z | 81.603° E | 38.968° | 2025-10-16 19:56:40.649Z | 162.152° S |
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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