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: 16 hours ago
TLE from 16 hours ago
0 QIANFAN-43
1 62244U 24232H 25287.95076478 .00000160 00000-0 22955-3 0 9994
2 62244 89.0026 47.1787 0015383 13.2776 346.8777 13.50978502 59922Epoch: 2025-10-14T22:49Z
TLE epoch observation values (Epoch: 2025-10-14T22:49:06.076Z)
Latitude
-0.00005°
Longitude
41.17155°
Altitude
1,060.456 km
Speed
7.327 km/s
True Right ascension
03h 08m 42s
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
09:05:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.163 km
Perigee altitude
1,054.261 km
Semi-major axis
7,443.849 km
Eccentricity
0.00154
Inclination
89.0026°
RAAN
47.1787°
Arg. of periapsis
13.2776°
True anomaly
346.8376°
Mean anomaly
346.8777°
Eccentric anomaly
346.85766°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00022955
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-15 18:58:30.493Z | 31.315° NE | 2025-10-15 19:03:30.493Z | 80.983° E | 19.783° | 2025-10-15 19:07:30.493Z | 121.232° SE |
| 11 mins | 2025-10-15 20:45:30.493Z | 349.697° N | 2025-10-15 20:50:30.493Z | 265.027° W | 41.077° | 2025-10-15 20:56:30.493Z | 197.991° SSW |
| 7 mins | 2025-10-16 06:58:30.493Z | 103.68° ESE | 2025-10-16 07:01:30.493Z | 72.398° E | 17.425° | 2025-10-16 07:05:30.493Z | 33.827° NE |
| 11 mins | 2025-10-16 08:42:30.493Z | 190.339° SSW | 2025-10-16 08:47:30.493Z | 286.735° WNW | 42.967° | 2025-10-16 08:53:30.493Z | 353.932° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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