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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-44
1 62245U 24232J 25339.93168445 .00000181 00000-0 26152-3 0 9993
2 62245 89.0034 41.7595 0013223 205.2286 154.8221 13.50977640 98419Epoch: 2025-12-05T22:21Z
TLE epoch observation values (Epoch: 2025-12-05T22:21:37.536Z)
Latitude
0°
Longitude
-8.61359°
Altitude
1,080.532 km
Speed
7.307 km/s
True Right ascension
02h 47m 02s
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
06:50:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.558 km
Perigee altitude
1,055.872 km
Semi-major axis
7,443.852 km
Eccentricity
0.00132
Inclination
89.0034°
RAAN
41.7595°
Arg. of periapsis
205.2286°
True anomaly
154.88647°
Mean anomaly
154.8221°
Eccentric anomaly
154.85429°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00026152
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-06 14:59:33.911Z | 47.584° ENE | 2025-12-06 15:02:33.911Z | 77.218° E | 15.199° | 2025-12-06 15:05:33.911Z | 106.16° ESE |
| 11 mins | 2025-12-06 16:44:33.911Z | 357.073° N | 2025-12-06 16:49:33.911Z | 283.638° WNW | 44.397° | 2025-12-06 16:55:33.911Z | 188.733° SSW |
| 4 mins | 2025-12-07 02:59:33.911Z | 84.575° E | 2025-12-07 03:00:33.911Z | 74.928° E | 13.553° | 2025-12-07 03:03:33.911Z | 46.626° ENE |
| 11 mins | 2025-12-07 04:41:33.911Z | 178.183° S | 2025-12-07 04:46:33.911Z | 282.52° WNW | 44.99° | 2025-12-07 04:52:33.911Z | 358.741° N |
| 4 mins | 2025-12-07 06:32:33.911Z | 272.784° WNW | 2025-12-07 06:33:33.911Z | 282.205° WNW | 12.703° | 2025-12-07 06:36:33.911Z | 309.908° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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