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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-41
1 62242U 24232F 25311.80356778 .00000228 00000-0 33560-3 0 9997
2 62242 89.0043 44.7146 0012120 293.1272 66.8602 13.50971604 94535Epoch: 2025-11-07T19:17Z
TLE epoch observation values (Epoch: 2025-11-07T19:17:08.256Z)
Latitude
0.00004°
Longitude
68.18791°
Altitude
1,068.101 km
Speed
7.32 km/s
True Right ascension
02h 58m 51s
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
22:36:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.759 km
Perigee altitude
1,056.715 km
Semi-major axis
7,443.874 km
Eccentricity
0.00121
Inclination
89.0043°
RAAN
44.7146°
Arg. of periapsis
293.1272°
True anomaly
66.98799°
Mean anomaly
66.8602°
Eccentric anomaly
66.92409°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.0003356
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-08 06:03:46.804Z | 146.753° SSE | 2025-11-08 06:08:46.804Z | 88.205° E | 34.284° | 2025-11-08 06:14:46.804Z | 14.249° NNE |
| 9 mins | 2025-11-08 07:51:46.804Z | 230.147° WSW | 2025-11-08 07:55:46.804Z | 279.549° WNW | 26.361° | 2025-11-08 08:00:46.804Z | 334.47° NNW |
| 8 mins | 2025-11-08 17:14:46.804Z | 42.569° NE | 2025-11-08 17:17:46.804Z | 74.446° E | 19.474° | 2025-11-08 17:22:46.804Z | 124.019° SE |
| 11 mins | 2025-11-08 18:59:46.804Z | 351.545° N | 2025-11-08 19:04:46.804Z | 288.403° WNW | 41.32° | 2025-11-08 19:10:46.804Z | 198.404° SSW |
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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