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 25260.91717679 .00000082 00000-0 10743-3 0 9991
2 62244 88.9977 49.9092 0017357 86.0272 274.2863 13.50967487 56271Epoch: 2025-09-17T22:00Z
TLE epoch observation values (Epoch: 2025-09-17T22:00:44.074Z)
Latitude
-0.00002°
Longitude
82.63931°
Altitude
1,070.71 km
Speed
7.317 km/s
True Right ascension
03h 19m 38s
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
23:08:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,078.673 km
Perigee altitude
1,052.832 km
Semi-major axis
7,443.889 km
Eccentricity
0.00174
Inclination
88.9977°
RAAN
49.9092°
Arg. of periapsis
86.0272°
True anomaly
274.08793°
Mean anomaly
274.2863°
Eccentric anomaly
274.18712°
Mean motion
3.37943 °/min
Orbital period
106.53 mins
BSTAR
0.00010743
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-18 08:50:07.980Z | 102.699° ESE | 2025-09-18 08:53:07.980Z | 74.655° E | 14.665° | 2025-09-18 08:56:07.980Z | 45.26° ENE |
| 11 mins | 2025-09-18 10:34:07.980Z | 182.339° SSW | 2025-09-18 10:39:07.980Z | 277.874° WNW | 44.685° | 2025-09-18 10:45:07.980Z | 356.953° N |
| 10 mins | 2025-09-18 21:44:07.980Z | 19.488° NNE | 2025-09-18 21:48:07.980Z | 74.309° E | 36.702° | 2025-09-18 21:54:07.980Z | 157.795° S |
| 8 mins | 2025-09-18 23:31:07.980Z | 325.611° NNW | 2025-09-18 23:35:07.980Z | 277.313° WNW | 23.615° | 2025-09-18 23:39:07.980Z | 235.073° WSW |
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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