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 26035.14593865 .00000021 00000-0 14266-4 0 9995
2 62245 89.0011 35.6778 0015083 45.1433 315.0941 13.50985355106546Epoch: 2026-02-04T03:30Z
TLE epoch observation values (Epoch: 2026-02-04T03:30:09.099Z)
Latitude
0.00003°
Longitude
-151.17683°
Altitude
1,063.64 km
Speed
7.324 km/s
True Right ascension
02h 22m 42s
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
12:24:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.914 km
Perigee altitude
1,054.459 km
Semi-major axis
7,443.823 km
Eccentricity
0.00151
Inclination
89.0011°
RAAN
35.6778°
Arg. of periapsis
45.1433°
True anomaly
314.97192°
Mean anomaly
315.0941°
Eccentric anomaly
315.03303°
Mean motion
3.37947 °/min
Orbital period
106.53 mins
BSTAR
0.000014266
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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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-02-04 11:13:09.497Z | 26.948° NE | 2026-02-04 11:18:09.497Z | 85.26° E | 26.68° | 2026-02-04 11:23:09.497Z | 138.882° SSE |
| 10 mins | 2026-02-04 13:00:09.497Z | 339.58° N | 2026-02-04 13:04:09.497Z | 288.064° WNW | 33.767° | 2026-02-04 13:10:09.497Z | 212.71° SW |
| 8 mins | 2026-02-04 23:12:09.497Z | 118.227° SE | 2026-02-04 23:15:09.497Z | 83.283° E | 23.821° | 2026-02-04 23:20:09.497Z | 27.208° NE |
| 10 mins | 2026-02-05 00:57:09.497Z | 206.797° SW | 2026-02-05 01:02:09.497Z | 284.505° WNW | 36.393° | 2026-02-05 01:07:09.497Z | 344.53° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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