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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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: 8 hours ago
TLE from 8 hours ago
0 QIANFAN-49
1 62250U 24232P 25339.95224686 .00000189 00000-0 27466-3 0 9998
2 62250 89.0033 41.9203 0013652 206.9712 153.0731 13.50977115 66925Epoch: 2025-12-05T22:51Z
TLE epoch observation values (Epoch: 2025-12-05T22:51:14.128Z)
Latitude
-0.00004°
Longitude
-15.87553°
Altitude
1,080.688 km
Speed
7.307 km/s
True Right ascension
02h 47m 40s
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
05:14:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,075.879 km
Perigee altitude
1,055.554 km
Semi-major axis
7,443.854 km
Eccentricity
0.00137
Inclination
89.0033°
RAAN
41.9203°
Arg. of periapsis
206.9712°
True anomaly
153.14384°
Mean anomaly
153.0731°
Eccentric anomaly
153.10848°
Mean motion
3.37945 °/min
Orbital period
106.53 mins
BSTAR
0.00027466
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-12-06 15:27:09.956Z | 25.782° NE | 2025-12-06 15:32:09.956Z | 77.443° E | 24.388° | 2025-12-06 15:37:09.956Z | 132.801° SE |
| 11 mins | 2025-12-06 17:14:09.956Z | 344.539° N | 2025-12-06 17:19:09.956Z | 276.407° WNW | 36.231° | 2025-12-06 17:25:09.956Z | 207.31° SW |
| 9 mins | 2025-12-07 03:26:09.956Z | 118.647° SE | 2025-12-07 03:30:09.956Z | 75.068° E | 22.235° | 2025-12-07 03:35:09.956Z | 25.601° NE |
| 11 mins | 2025-12-07 05:11:09.956Z | 200.581° SSW | 2025-12-07 05:16:09.956Z | 272.517° WNW | 39.049° | 2025-12-07 05:22:09.956Z | 348.565° 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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