QIANFAN-43, 62244
Orbit data source: Space-Track
QIANFAN-43, 62244 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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62244 intel report (Beta)
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Edit Public Description
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: 14 hours ago
TLE from 14 hours ago
0 QIANFAN-43
1 62244U 24232H 25297.20879414 .00000199 00000-0 28958-3 0 9995
2 62244 89.0038 46.2465 0014503 345.6549 14.4188 13.50981534 61174Epoch: 2025-10-24T05:00Z
TLE epoch observation values (Epoch: 2025-10-24T05:00:39.813Z)
Latitude
-0.00007°
Longitude
-61.77638°
Altitude
1,061.142 km
Speed
7.326 km/s
True Right ascension
03h 04m 59s
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
14:27:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.496 km
Perigee altitude
1,054.905 km
Semi-major axis
7,443.837 km
Eccentricity
0.00145
Inclination
89.0038°
RAAN
46.2465°
Arg. of periapsis
345.6549°
True anomaly
14.46026°
Mean anomaly
14.4188°
Eccentric anomaly
14.43952°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00028958
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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-43 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-24 19:49:11.997Z | 358.293° N | 2025-10-24 19:55:11.997Z | 289.437° WNW | 44.558° | 2025-10-24 20:01:11.997Z | 187.853° SSW |
| 4 mins | 2025-10-25 06:05:11.997Z | 84.722° E | 2025-10-25 06:07:11.997Z | 65.37° ENE | 12.934° | 2025-10-25 06:09:11.997Z | 47.004° ENE |
| 11 mins | 2025-10-25 07:47:11.997Z | 177.111° S | 2025-10-25 07:52:11.997Z | 135.42° SSE | 44.999° | 2025-10-25 07:58:11.997Z | 359.236° N |
| 4 mins | 2025-10-25 09:38:11.997Z | 272.295° WNW | 2025-10-25 09:39:11.997Z | 281.858° WNW | 12.813° | 2025-10-25 09:42:11.997Z | 309.961° NW |
| 10 mins | 2025-10-25 18:57:11.997Z | 21.527° NNE | 2025-10-25 19:02:11.997Z | 95.524° ESE | 34.505° | 2025-10-25 19:07:11.997Z | 152.907° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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