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: 12 hours ago
TLE from 12 hours ago
0 QIANFAN-41
1 62242U 24232F 25257.58833716 .00000055 00000-0 65715-4 0 9999
2 62242 88.9967 50.1850 0015893 89.9084 270.3889 13.50969639 87214Epoch: 2025-09-14T14:07Z
TLE epoch observation values (Epoch: 2025-09-14T14:07:12.33Z)
Latitude
0.00004°
Longitude
-155.42156°
Altitude
1,071.585 km
Speed
7.316 km/s
True Right ascension
03h 20m 44s
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
19:13:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.575 km
Perigee altitude
1,053.914 km
Semi-major axis
7,443.881 km
Eccentricity
0.00159
Inclination
88.9967°
RAAN
50.185°
Arg. of periapsis
89.9084°
True anomaly
270.20678°
Mean anomaly
270.3889°
Eccentric anomaly
270.29784°
Mean motion
3.37943 °/min
Orbital period
106.53 mins
BSTAR
0.000065715
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-09-15 09:47:30.707Z | 138.64° SSE | 2025-09-15 09:52:30.707Z | 79.262° E | 30.202° | 2025-09-15 09:57:30.707Z | 20.284° NNE |
| 10 mins | 2025-09-15 11:34:30.707Z | 219.714° SW | 2025-09-15 11:38:30.707Z | 268.329° W | 29.968° | 2025-09-15 11:44:30.707Z | 339.988° N |
| 6 mins | 2025-09-15 20:58:30.707Z | 49.57° ENE | 2025-09-15 21:01:30.707Z | 80.45° E | 15.918° | 2025-09-15 21:04:30.707Z | 109.418° ESE |
| 11 mins | 2025-09-15 22:43:30.707Z | 355.356° N | 2025-09-15 22:48:30.707Z | 256.131° W | 43.867° | 2025-09-15 22:54:30.707Z | 190.421° 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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