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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-40
1 62241U 24232E 26246.82537599 .00000116 00000-0 16008-3 0 9992
2 62241 89.0171 14.2924 0014786 151.2471 208.9499 13.51026652135384Epoch: 2026-09-03T19:48Z
TLE epoch observation values (Epoch: 2026-09-03T19:48:32.485Z)
Latitude
0.00005°
Longitude
94.19905°
Altitude
1,081.077 km
Speed
7.307 km/s
True Right ascension
00h 57m 10s
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
20:53:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.541 km
Perigee altitude
1,054.528 km
Semi-major axis
7,443.672 km
Eccentricity
0.00148
Inclination
89.0171°
RAAN
14.2924°
Arg. of periapsis
151.2471°
True anomaly
208.86802°
Mean anomaly
208.9499°
Eccentric anomaly
208.90895°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.00016008
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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 | 2026-09-04 08:21:47.627Z | 148.689° SSE | 2026-09-04 08:26:47.627Z | 89.488° E | 35.385° | 2026-09-04 08:32:47.627Z | 13.376° NNE |
| 9 mins | 2026-09-04 10:09:47.627Z | 231.479° WSW | 2026-09-04 10:13:47.627Z | 279.104° WNW | 25.308° | 2026-09-04 10:18:47.627Z | 333.422° NNW |
| 8 mins | 2026-09-04 19:32:47.627Z | 42.504° NE | 2026-09-04 19:35:47.627Z | 75.469° E | 20.032° | 2026-09-04 19:40:47.627Z | 125.92° SE |
| 11 mins | 2026-09-04 21:17:47.627Z | 350.251° N | 2026-09-04 21:22:47.627Z | 283.247° WNW | 40.49° | 2026-09-04 21:28:47.627Z | 199.939° SSW |
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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