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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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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-44
1 62245U 24232J 26246.81716510 .00000077 00000-0 10111-3 0 9992
2 62245 89.0143 14.4647 0015108 142.6546 217.5658 13.51027575135127Epoch: 2026-09-03T19:36Z
TLE epoch observation values (Epoch: 2026-09-03T19:36:43.064Z)
Latitude
-0.00007°
Longitude
97.33536°
Altitude
1,080.359 km
Speed
7.308 km/s
True Right ascension
00h 57m 51s
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
20:53:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.777 km
Perigee altitude
1,054.285 km
Semi-major axis
7,443.668 km
Eccentricity
0.00151
Inclination
89.0143°
RAAN
14.4647°
Arg. of periapsis
142.6546°
True anomaly
217.46041°
Mean anomaly
217.5658°
Eccentric anomaly
217.51309°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.00010111
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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 | 2026-09-04 08:09:54.593Z | 141.574° SSE | 2026-09-04 08:14:54.593Z | 88.895° E | 30.512° | 2026-09-04 08:20:54.593Z | 17.63° NNE |
| 10 mins | 2026-09-04 09:56:54.593Z | 217.482° SW | 2026-09-04 10:01:54.593Z | 277.886° WNW | 29.897° | 2026-09-04 10:06:54.593Z | 336.999° NNW |
| 6 mins | 2026-09-04 19:21:54.593Z | 53.99° ENE | 2026-09-04 19:23:54.593Z | 74.965° E | 16.206° | 2026-09-04 19:27:54.593Z | 113.634° SE |
| 11 mins | 2026-09-04 21:05:54.593Z | 355.608° N | 2026-09-04 21:10:54.593Z | 295.903° NW | 43.589° | 2026-09-04 21:16:54.593Z | 191.611° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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