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: 16 hours ago
TLE from 16 hours ago
0 QIANFAN-44
1 62245U 24232J 25287.93835580 .00000150 00000-0 21405-3 0 9998
2 62245 89.0024 46.9916 0013530 11.2333 348.9118 13.50979798 91398Epoch: 2025-10-14T22:31Z
TLE epoch observation values (Epoch: 2025-10-14T22:31:13.941Z)
Latitude
0.00004°
Longitude
45.46391°
Altitude
1,061.72 km
Speed
7.326 km/s
True Right ascension
03h 07m 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
09:07:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.778 km
Perigee altitude
1,055.635 km
Semi-major axis
7,443.844 km
Eccentricity
0.00135
Inclination
89.0024°
RAAN
46.9916°
Arg. of periapsis
11.2333°
True anomaly
348.88193°
Mean anomaly
348.9118°
Eccentric anomaly
348.89687°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00021405
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-15 18:41:38.588Z | 42.165° NE | 2025-10-15 18:45:38.588Z | 79.91° E | 14.61° | 2025-10-15 18:48:38.588Z | 107.511° ESE |
| 11 mins | 2025-10-15 20:27:38.588Z | 358.016° N | 2025-10-15 20:32:38.588Z | 246.989° WSW | 44.633° | 2025-10-15 20:38:38.588Z | 186.956° SSW |
| 11 mins | 2025-10-16 08:24:38.588Z | 176.256° S | 2025-10-16 08:29:38.588Z | 15.048° NNE | 44.837° | 2025-10-16 08:35:38.588Z | 359.648° N |
| 4 mins | 2025-10-16 10:15:38.588Z | 274.666° WNW | 2025-10-16 10:16:38.588Z | 284.425° WNW | 13.114° | 2025-10-16 10:19:38.588Z | 312.366° NW |
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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