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: 5 hours ago
TLE from 5 hours ago
0 QIANFAN-44
1 62245U 24232J 25355.41116639 .00000089 00000-0 11957-3 0 9996
2 62245 89.0019 40.1989 0014592 161.3750 198.7938 13.50980926100507Epoch: 2025-12-21T09:52Z
TLE epoch observation values (Epoch: 2025-12-21T09:52:04.776Z)
Latitude
-0.00001°
Longitude
161.955°
Altitude
1,081.896 km
Speed
7.306 km/s
True Right ascension
02h 40m 47s
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
14:21:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.565 km
Perigee altitude
1,054.841 km
Semi-major axis
7,443.84 km
Eccentricity
0.00146
Inclination
89.0019°
RAAN
40.1989°
Arg. of periapsis
161.375°
True anomaly
198.74002°
Mean anomaly
198.7938°
Eccentric anomaly
198.7669°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00011957
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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 | 2025-12-21 15:47:03.703Z | 355.181° N | 2025-12-21 15:53:03.703Z | 295.885° NW | 42.39° | 2025-12-21 15:59:03.703Z | 195.164° SSW |
| 6 mins | 2025-12-22 02:02:03.703Z | 98.717° ESE | 2025-12-22 02:05:03.703Z | 68.405° E | 15.925° | 2025-12-22 02:08:03.703Z | 39.821° NE |
| 11 mins | 2025-12-22 03:45:03.703Z | 184.729° SSW | 2025-12-22 03:50:03.703Z | 237.652° WSW | 43.963° | 2025-12-22 03:56:03.703Z | 355.124° N |
| 11 mins | 2025-12-22 14:55:03.703Z | 15.661° NNE | 2025-12-22 15:00:03.703Z | 89.904° E | 38.293° | 2025-12-22 15:06:03.703Z | 161.895° S |
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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