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: 13 hours ago
TLE from 13 hours ago
0 QIANFAN-49
1 62250U 24232P 26171.44228992 .00000057 00000-0 69878-4 0 9999
2 62250 89.0076 22.1764 0014716 15.0442 345.1144 13.51012406 93450Epoch: 2026-06-20T10:36Z
TLE epoch observation values (Epoch: 2026-06-20T10:36:53.849Z)
Latitude
0.00001°
Longitude
-45.70482°
Altitude
1,060.897 km
Speed
7.327 km/s
True Right ascension
01h 28m 42s
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
10:18:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.541 km
Perigee altitude
1,054.633 km
Semi-major axis
7,443.724 km
Eccentricity
0.00147
Inclination
89.0076°
RAAN
22.1764°
Arg. of periapsis
15.0442°
True anomaly
345.071°
Mean anomaly
345.1144°
Eccentric anomaly
345.09271°
Mean motion
3.37954 °/min
Orbital period
106.52 mins
BSTAR
0.000069878
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-21 01:25:44.490Z | 20.824° NNE | 2026-06-21 01:31:44.490Z | 89.527° E | 28.877° | 2026-06-21 01:36:44.490Z | 143.27° SSE |
| 10 mins | 2026-06-21 03:13:44.490Z | 335.741° NNW | 2026-06-21 03:17:44.490Z | 282.506° WNW | 31.767° | 2026-06-21 03:23:44.490Z | 215.324° SW |
| 9 mins | 2026-06-21 13:24:44.490Z | 126.712° SE | 2026-06-21 13:28:44.490Z | 79.502° E | 26.11° | 2026-06-21 13:33:44.490Z | 23.835° NE |
| 10 mins | 2026-06-21 15:10:44.490Z | 212.471° SW | 2026-06-21 15:14:44.490Z | 265.918° W | 34.178° | 2026-06-21 15:20:44.490Z | 343.482° 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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