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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-41
1 62242U 24232F 25339.94812930 .00000189 00000-0 27430-3 0 9994
2 62242 89.0032 41.8819 0013576 202.9975 157.0570 13.50976421 98333Epoch: 2025-12-05T22:45Z
TLE epoch observation values (Epoch: 2025-12-05T22:45:18.371Z)
Latitude
-0.00002°
Longitude
-14.42755°
Altitude
1,080.935 km
Speed
7.307 km/s
True Right ascension
02h 47m 31s
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
05:09:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.825 km
Perigee altitude
1,055.613 km
Semi-major axis
7,443.856 km
Eccentricity
0.00136
Inclination
89.0032°
RAAN
41.8819°
Arg. of periapsis
202.9975°
True anomaly
157.11755°
Mean anomaly
157.057°
Eccentric anomaly
157.08728°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.0002743
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-06 15:21:51.797Z | 31.327° NE | 2025-12-06 15:26:51.797Z | 86.094° E | 22.255° | 2025-12-06 15:30:51.797Z | 127.546° SE |
| 10 mins | 2025-12-06 17:08:51.797Z | 344.346° N | 2025-12-06 17:12:51.797Z | 288.145° WNW | 38.114° | 2025-12-06 17:18:51.797Z | 204.863° SW |
| 8 mins | 2025-12-07 03:20:51.797Z | 111.536° ESE | 2025-12-07 03:23:51.797Z | 79.859° E | 20.252° | 2025-12-07 03:28:51.797Z | 29.349° NE |
| 11 mins | 2025-12-07 05:04:51.797Z | 195.206° SSW | 2025-12-07 05:09:51.797Z | 256.927° W | 40.655° | 2025-12-07 05:15:51.797Z | 349.575° 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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