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: 15 hours ago
TLE from 15 hours ago
0 QIANFAN-44
1 62245U 24232J 25261.20107395 .00000073 00000-0 93471-4 0 9993
2 62245 88.9976 49.6925 0015549 82.8247 277.4671 13.50972923 87783Epoch: 2025-09-18T04:49Z
TLE epoch observation values (Epoch: 2025-09-18T04:49:32.789Z)
Latitude
-0.00005°
Longitude
-20.06019°
Altitude
1,070.147 km
Speed
7.318 km/s
True Right ascension
03h 18m 46s
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
12:48:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.307 km
Perigee altitude
1,054.158 km
Semi-major axis
7,443.869 km
Eccentricity
0.00155
Inclination
88.9976°
RAAN
49.6925°
Arg. of periapsis
82.8247°
True anomaly
277.29039°
Mean anomaly
277.4671°
Eccentric anomaly
277.37875°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.000093471
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-18 21:25:25.404Z | 21.343° NNE | 2025-09-18 21:30:25.404Z | 78.645° E | 30.432° | 2025-09-18 21:36:25.404Z | 147.719° SSE |
| 10 mins | 2025-09-18 23:12:25.404Z | 337.757° N | 2025-09-18 23:17:25.404Z | 274.783° WNW | 29.836° | 2025-09-18 23:22:25.404Z | 220.243° SW |
| 9 mins | 2025-09-19 09:24:25.404Z | 126.681° SE | 2025-09-19 09:28:25.404Z | 74.109° E | 27.677° | 2025-09-19 09:33:25.404Z | 20.811° NNE |
| 11 mins | 2025-09-19 11:09:25.404Z | 211.732° SW | 2025-09-19 11:14:25.404Z | 273.692° WNW | 32.673° | 2025-09-19 11:20:25.404Z | 343.364° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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