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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-41
1 62242U 24232F 26126.77833294 .00000157 00000-0 22426-3 0 9991
2 62242 89.0112 26.6090 0015205 125.7522 234.5045 13.51006124118836Epoch: 2026-05-06T18:40Z
TLE epoch observation values (Epoch: 2026-05-06T18:40:47.966Z)
Latitude
-0.00006°
Longitude
-118.2248°
Altitude
1,078.1 km
Speed
7.31 km/s
True Right ascension
01h 46m 26s
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
10:25:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.928 km
Perigee altitude
1,054.292 km
Semi-major axis
7,443.747 km
Eccentricity
0.00152
Inclination
89.0112°
RAAN
26.609°
Arg. of periapsis
125.7522°
True anomaly
234.3628°
Mean anomaly
234.5045°
Eccentric anomaly
234.43363°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.00022426
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-07 04:11:28.271Z | 40.941° NE | 2026-05-07 04:15:28.271Z | 83.028° E | 18.032° | 2026-05-07 04:18:28.271Z | 113.5° SE |
| 11 mins | 2026-05-07 05:57:28.271Z | 351.288° N | 2026-05-07 06:02:28.271Z | 253.454° W | 41.927° | 2026-05-07 06:08:28.271Z | 194.938° SSW |
| 6 mins | 2026-05-07 16:10:28.271Z | 101.105° ESE | 2026-05-07 16:13:28.271Z | 70.759° E | 16.319° | 2026-05-07 16:16:28.271Z | 41.211° NE |
| 12 mins | 2026-05-07 17:53:28.271Z | 185.603° SSW | 2026-05-07 17:59:28.271Z | 302.621° NW | 43.572° | 2026-05-07 18:05:28.271Z | 355.491° 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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