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 26171.42994688 .00000069 00000-0 88471-4 0 9992
2 62241 89.0104 21.8257 0014389 23.1316 337.0480 13.51008002125200Epoch: 2026-06-20T10:19Z
TLE epoch observation values (Epoch: 2026-06-20T10:19:07.410Z)
Latitude
-0.00001°
Longitude
-41.59986°
Altitude
1,061.639 km
Speed
7.326 km/s
True Right ascension
01h 27m 18s
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
07:22:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.314 km
Perigee altitude
1,054.892 km
Semi-major axis
7,443.74 km
Eccentricity
0.00144
Inclination
89.0104°
RAAN
21.8257°
Arg. of periapsis
23.1316°
True anomaly
336.98359°
Mean anomaly
337.048°
Eccentric anomaly
337.01581°
Mean motion
3.37953 °/min
Orbital period
106.52 mins
BSTAR
0.000088471
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-21 01:08:57.105Z | 31.415° NE | 2026-06-21 01:12:57.105Z | 73.301° E | 22.94° | 2026-06-21 01:17:57.105Z | 128.643° SE |
| 11 mins | 2026-06-21 02:54:57.105Z | 347.319° N | 2026-06-21 02:59:57.105Z | 285.555° WNW | 37.746° | 2026-06-21 03:05:57.105Z | 205.714° SW |
| 8 mins | 2026-06-21 13:07:57.105Z | 111.993° ESE | 2026-06-21 13:10:57.105Z | 79.504° E | 20.457° | 2026-06-21 13:15:57.105Z | 28.571° NE |
| 11 mins | 2026-06-21 14:51:57.105Z | 196.381° SSW | 2026-06-21 14:56:57.105Z | 259.156° W | 40.065° | 2026-06-21 15:02:57.105Z | 349.143° 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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