QIANFAN-49, 62250
Orbit data source: Space-Track
QIANFAN-49, 62250 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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62250 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: 10 hours ago
TLE from 10 hours ago
0 QIANFAN-49
1 62250U 24232P 26307.56832293 .00000071 00000-0 91959-4 0 9999
2 62250 89.0156 8.5833 0012964 340.9420 19.1244 13.51034981111837Epoch: 2026-11-03T13:38Z
TLE epoch observation values (Epoch: 2026-11-03T13:38:23.101Z)
Latitude
-0.00005°
Longitude
121.15792°
Altitude
1,062.285 km
Speed
7.325 km/s
True Right ascension
00h 34m 19s
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
19:45:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.154 km
Perigee altitude
1,055.854 km
Semi-major axis
7,443.641 km
Eccentricity
0.0013
Inclination
89.0156°
RAAN
8.5833°
Arg. of periapsis
340.942°
True anomaly
19.17314°
Mean anomaly
19.1244°
Eccentric anomaly
19.14876°
Mean motion
3.3796 °/min
Orbital period
106.52 mins
BSTAR
0.000091959
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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-49 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 | 2026-11-04 03:57:22.491Z | 151.081° SSE | 2026-11-04 04:03:22.491Z | 85.297° E | 44.626° | 2026-11-04 04:09:22.491Z | 13.132° NNE |
| 9 mins | 2026-11-04 05:46:22.491Z | 232.223° WSW | 2026-11-04 05:50:22.491Z | 281.635° WNW | 28.553° | 2026-11-04 05:55:22.491Z | 334.662° NNW |
| 8 mins | 2026-11-04 15:09:22.491Z | 43.416° NE | 2026-11-04 15:12:22.491Z | 76.222° E | 21.579° | 2026-11-04 15:17:22.491Z | 125.745° SE |
| 11 mins | 2026-11-04 16:54:22.491Z | 350.371° N | 2026-11-04 16:59:22.491Z | 281.18° WNW | 60.102° | 2026-11-04 17:05:22.491Z | 199.378° 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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