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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-43
1 62244U 24232H 25339.94395861 .00000190 00000-0 27537-3 0 9995
2 62244 89.0036 41.9474 0014905 209.1969 150.8350 13.50975293 66941Epoch: 2025-12-05T22:39Z
TLE epoch observation values (Epoch: 2025-12-05T22:39:18.023Z)
Latitude
-0.00009°
Longitude
-12.85649°
Altitude
1,081.324 km
Speed
7.307 km/s
True Right ascension
02h 47m 47s
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
05:07:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.818 km
Perigee altitude
1,054.628 km
Semi-major axis
7,443.86 km
Eccentricity
0.00149
Inclination
89.0036°
RAAN
41.9474°
Arg. of periapsis
209.1969°
True anomaly
150.9181°
Mean anomaly
150.835°
Eccentric anomaly
150.87656°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00027537
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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 | 2025-12-06 15:15:49.089Z | 32.615° NE | 2025-12-06 15:19:49.089Z | 72.149° E | 20.205° | 2025-12-06 15:24:49.089Z | 124.337° SE |
| 10 mins | 2025-12-06 17:02:49.089Z | 347.652° N | 2025-12-06 17:06:49.089Z | 293.167° NW | 40.053° | 2025-12-06 17:12:49.089Z | 200.925° SSW |
| 7 mins | 2025-12-07 03:15:49.089Z | 101.189° ESE | 2025-12-07 03:18:49.089Z | 68.475° E | 18.342° | 2025-12-07 03:22:49.089Z | 31.182° NE |
| 12 mins | 2025-12-07 04:58:49.089Z | 190.594° SSW | 2025-12-07 05:03:49.089Z | 249.367° W | 42.311° | 2025-12-07 05:10:49.089Z | 353.695° 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
Authenticating...
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