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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-40
1 62241U 24232E 26305.11195473 .00000082 00000-0 10856-3 0 9998
2 62241 89.0186 8.5136 0012867 357.5155 2.5930 13.51026346143252Epoch: 2026-11-01T02:41Z
TLE epoch observation values (Epoch: 2026-11-01T02:41:12.888Z)
Latitude
-0.00004°
Longitude
-72.19811°
Altitude
1,061.864 km
Speed
7.326 km/s
True Right ascension
00h 34m 03s
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
06:20:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.113 km
Perigee altitude
1,055.958 km
Semi-major axis
7,443.673 km
Eccentricity
0.00129
Inclination
89.0186°
RAAN
8.5136°
Arg. of periapsis
357.5155°
True anomaly
2.59968°
Mean anomaly
2.593°
Eccentric anomaly
2.59634°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.00010856
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-11-01 15:43:19.723Z | 20.577° NNE | 2026-11-01 15:49:19.723Z | 87.204° E | 33.121° | 2026-11-01 15:54:19.723Z | 142.045° SSE |
| 10 mins | 2026-11-01 17:31:19.723Z | 336.903° NNW | 2026-11-01 17:35:19.723Z | 285.147° WNW | 38.95° | 2026-11-01 17:41:19.723Z | 215.294° SW |
| 9 mins | 2026-11-02 03:42:19.723Z | 126.496° SE | 2026-11-02 03:46:19.723Z | 80.259° E | 28.983° | 2026-11-02 03:51:19.723Z | 24.462° NE |
| 10 mins | 2026-11-02 05:28:19.723Z | 211.533° SW | 2026-11-02 05:32:19.723Z | 264.561° W | 43.585° | 2026-11-02 05:38:19.723Z | 343.555° 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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