QIANFAN-44, 62245
Orbit data source: Space-Track
QIANFAN-44, 62245 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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62245 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-44
1 62245U 24232J 25323.78557948 .00000121 00000-0 16855-3 0 9992
2 62245 89.0047 43.3847 0012034 255.8703 104.1111 13.50972246 96236Epoch: 2025-11-19T18:51Z
TLE epoch observation values (Epoch: 2025-11-19T18:51:14.067Z)
Latitude
-0.00001°
Longitude
61.52376°
Altitude
1,073.832 km
Speed
7.314 km/s
True Right ascension
02h 53m 32s
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
22:31:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.693 km
Perigee altitude
1,056.777 km
Semi-major axis
7,443.872 km
Eccentricity
0.0012
Inclination
89.0047°
RAAN
43.3847°
Arg. of periapsis
255.8703°
True anomaly
104.24479°
Mean anomaly
104.1111°
Eccentric anomaly
104.17795°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00016855
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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-44 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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-11-20 05:36:39.861Z | 166.742° S | 2025-11-20 05:42:39.861Z | 106.425° ESE | 42.818° | 2025-11-20 05:48:39.861Z | 5.36° NNE |
| 6 mins | 2025-11-20 07:27:39.861Z | 256.867° W | 2025-11-20 07:29:39.861Z | 277.858° WNW | 17.485° | 2025-11-20 07:33:39.861Z | 318.699° NNW |
| 10 mins | 2025-11-20 16:47:39.861Z | 25.508° NE | 2025-11-20 16:52:39.861Z | 86.198° E | 28.619° | 2025-11-20 16:57:39.861Z | 141.868° SSE |
| 10 mins | 2025-11-20 18:34:39.861Z | 337.256° NNW | 2025-11-20 18:38:39.861Z | 286.44° WNW | 31.946° | 2025-11-20 18:44:39.861Z | 215.555° SW |
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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