QIANFAN-40, 62241
Orbit data source: Space-Track
QIANFAN-40, 62241 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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62241 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-40
1 62241U 24232E 26096.92275375 .00000176 00000-0 25368-3 0 9992
2 62241 89.0137 29.2595 0011612 226.1155 133.9038 13.51010179115147Epoch: 2026-04-06T22:08Z
TLE epoch observation values (Epoch: 2026-04-06T22:08:45.923Z)
Latitude
-0.00005°
Longitude
-138.13872°
Altitude
1,077.5 km
Speed
7.31 km/s
True Right ascension
01h 57m 02s
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
14:01:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.239 km
Perigee altitude
1,056.951 km
Semi-major axis
7,443.732 km
Eccentricity
0.00116
Inclination
89.0137°
RAAN
29.2595°
Arg. of periapsis
226.1155°
True anomaly
133.99958°
Mean anomaly
133.9038°
Eccentric anomaly
133.9517°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.00025368
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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-40 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 | 2026-04-07 09:25:53.584Z | 319.963° NNW | 2026-04-07 09:28:53.584Z | 291.708° WNW | 15.326° | 2026-04-07 09:32:53.584Z | 253.824° W |
| 12 mins | 2026-04-07 19:34:53.584Z | 165.945° S | 2026-04-07 19:40:53.584Z | 58.517° ENE | 42.757° | 2026-04-07 19:46:53.584Z | 4.173° NNE |
| 7 mins | 2026-04-07 21:24:53.584Z | 255.236° W | 2026-04-07 21:27:53.584Z | 286.993° WNW | 17.408° | 2026-04-07 21:31:53.584Z | 324.639° NNW |
| 9 mins | 2026-04-08 06:45:53.584Z | 31.014° NE | 2026-04-08 06:49:53.584Z | 83.46° E | 28.734° | 2026-04-08 06:54:53.584Z | 141.278° SSE |
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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