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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-43
1 62244U 24232H 25311.79941292 .00000143 00000-0 20379-3 0 9998
2 62244 89.0047 44.7787 0013676 299.0326 60.9454 13.50985253 63142Epoch: 2025-11-07T19:11Z
TLE epoch observation values (Epoch: 2025-11-07T19:11:09.276Z)
Latitude
-0.00006°
Longitude
69.75186°
Altitude
1,066.653 km
Speed
7.321 km/s
True Right ascension
02h 59m 06s
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
22:18:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.867 km
Perigee altitude
1,055.507 km
Semi-major axis
7,443.824 km
Eccentricity
0.00137
Inclination
89.0047°
RAAN
44.7787°
Arg. of periapsis
299.0326°
True anomaly
61.08251°
Mean anomaly
60.9454°
Eccentric anomaly
61.01394°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.00020379
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-08 05:57:46.028Z | 143.149° SSE | 2025-11-08 06:02:46.028Z | 87.896° E | 31.859° | 2025-11-08 06:08:46.028Z | 16.321° NNE |
| 9 mins | 2025-11-08 07:45:46.028Z | 226.454° WSW | 2025-11-08 07:49:46.028Z | 279.178° WNW | 28.647° | 2025-11-08 07:54:46.028Z | 336.286° NNW |
| 7 mins | 2025-11-08 17:08:46.028Z | 43.858° NE | 2025-11-08 17:11:46.028Z | 74.313° E | 17.592° | 2025-11-08 17:15:46.028Z | 114.287° SE |
| 11 mins | 2025-11-08 18:53:46.028Z | 354.173° N | 2025-11-08 18:58:46.028Z | 294.778° NW | 42.855° | 2025-11-08 19:04:46.028Z | 194.187° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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