QIANFAN-41, 62242
Orbit data source: Space-Track
QIANFAN-41, 62242 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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62242 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: 19 hours ago
TLE from 19 hours ago
0 QIANFAN-41
1 62242U 24232F 25341.28129312 .00000211 00000-0 30896-3 0 9995
2 62242 89.0031 41.7476 0013693 199.0920 160.9720 13.50976951 98514Epoch: 2025-12-07T06:45Z
TLE epoch observation values (Epoch: 2025-12-07T06:45:03.725Z)
Latitude
0.00001°
Longitude
-135.81485°
Altitude
1,081.263 km
Speed
7.307 km/s
True Right ascension
02h 46m 59s
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
23:44:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.91 km
Perigee altitude
1,055.524 km
Semi-major axis
7,443.854 km
Eccentricity
0.00137
Inclination
89.0031°
RAAN
41.7476°
Arg. of periapsis
199.092°
True anomaly
161.02307°
Mean anomaly
160.972°
Eccentric anomaly
160.99755°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00030896
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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-41 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 | 2025-12-08 04:10:20.492Z | 161.446° S | 2025-12-08 04:16:20.492Z | 102.796° ESE | 40.299° | 2025-12-08 04:22:20.492Z | 8.893° NNE |
| 8 mins | 2025-12-08 06:00:20.492Z | 244.17° WSW | 2025-12-08 06:03:20.492Z | 276.168° WNW | 20.245° | 2025-12-08 06:08:20.492Z | 327.568° NNW |
| 9 mins | 2025-12-08 15:22:20.492Z | 35.119° NE | 2025-12-08 15:26:20.492Z | 84.775° E | 25.238° | 2025-12-08 15:31:20.492Z | 136.966° SSE |
| 10 mins | 2025-12-08 17:08:20.492Z | 341.248° N | 2025-12-08 17:12:20.492Z | 289.347° WNW | 35.001° | 2025-12-08 17:18:20.492Z | 210.511° SW |
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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