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 25346.98010368 .00000119 00000-0 16645-3 0 9992
2 62244 89.0031 41.2385 0015545 188.6241 171.4646 13.50977313 67892Epoch: 2025-12-12T23:31Z
TLE epoch observation values (Epoch: 2025-12-12T23:31:20.957Z)
Latitude
0.00001°
Longitude
-33.51277°
Altitude
1,083.069 km
Speed
7.305 km/s
True Right ascension
02h 44m 57s
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
05:21:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.287 km
Perigee altitude
1,054.145 km
Semi-major axis
7,443.853 km
Eccentricity
0.00155
Inclination
89.0031°
RAAN
41.2385°
Arg. of periapsis
188.6241°
True anomaly
171.49099°
Mean anomaly
171.4646°
Eccentric anomaly
171.4778°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00016645
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-13 14:23:16.238Z | 54.384° ENE | 2025-12-13 14:25:16.238Z | 73.448° E | 13.124° | 2025-12-13 14:28:16.238Z | 101.262° ESE |
| 12 mins | 2025-12-13 16:07:16.238Z | 0.424° NNE | 2025-12-13 16:12:16.238Z | 352.945° N | 44.469° | 2025-12-13 16:19:16.238Z | 183.673° SSW |
| 12 mins | 2025-12-14 04:04:16.238Z | 172.591° S | 2025-12-14 04:09:16.238Z | 133.156° SE | 44.379° | 2025-12-14 04:16:16.238Z | 1.184° NNE |
| 5 mins | 2025-12-14 05:55:16.238Z | 268.158° W | 2025-12-14 05:57:16.238Z | 288.304° WNW | 14.714° | 2025-12-14 06:00:16.238Z | 316.254° NNW |
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
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