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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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-41
1 62242U 24232F 26305.19399979 .00000077 00000-0 10086-3 0 9993
2 62242 89.0157 8.7764 0012809 344.3691 15.7063 13.51038882142929Epoch: 2026-11-01T04:39Z
TLE epoch observation values (Epoch: 2026-11-01T04:39:21.581Z)
Latitude
-0.00004°
Longitude
-101.5524°
Altitude
1,062.209 km
Speed
7.325 km/s
True Right ascension
00h 35m 06s
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
06:22:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.024 km
Perigee altitude
1,055.955 km
Semi-major axis
7,443.627 km
Eccentricity
0.00128
Inclination
89.0157°
RAAN
8.7764°
Arg. of periapsis
344.3691°
True anomaly
15.7461°
Mean anomaly
15.7063°
Eccentric anomaly
15.72619°
Mean motion
3.37961 °/min
Orbital period
106.52 mins
BSTAR
0.00010086
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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 | 2026-11-01 15:54:43.478Z | 17.015° NNE | 2026-11-01 16:00:43.478Z | 86.081° E | 39.885° | 2026-11-01 16:06:43.478Z | 152.041° SSE |
| 10 mins | 2026-11-01 17:42:43.478Z | 333.57° NNW | 2026-11-01 17:46:43.478Z | 285.951° WNW | 32.57° | 2026-11-01 17:52:43.478Z | 221.347° SW |
| 10 mins | 2026-11-02 03:53:43.478Z | 132.654° SE | 2026-11-02 03:57:43.478Z | 81.952° E | 34.764° | 2026-11-02 04:03:43.478Z | 16.934° NNE |
| 10 mins | 2026-11-02 05:39:43.478Z | 217.906° SW | 2026-11-02 05:44:43.478Z | 284.856° WNW | 36.377° | 2026-11-02 05:49:43.478Z | 339.721° N |
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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