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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-49
1 62250U 24232P 25312.47426131 .00000215 00000-0 31487-3 0 9993
2 62250 89.0045 44.6856 0012329 295.2061 64.7812 13.50972253 63215Epoch: 2025-11-08T11:22Z
TLE epoch observation values (Epoch: 2025-11-08T11:22:56.177Z)
Latitude
0.00005°
Longitude
-173.95182°
Altitude
1,067.733 km
Speed
7.32 km/s
True Right ascension
02h 58m 44s
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
16:17:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,074.912 km
Perigee altitude
1,056.557 km
Semi-major axis
7,443.872 km
Eccentricity
0.00123
Inclination
89.0045°
RAAN
44.6856°
Arg. of periapsis
295.2061°
True anomaly
64.9091°
Mean anomaly
64.7812°
Eccentric anomaly
64.84514°
Mean motion
3.37944 °/min
Orbital period
106.53 mins
BSTAR
0.00031487
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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
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-11-09 05:18:07.061Z | 113.515° SE | 2025-11-09 05:22:07.061Z | 72.812° E | 19.072° | 2025-11-09 05:26:07.061Z | 33.108° NE |
| 11 mins | 2025-11-09 07:03:07.061Z | 194.018° SSW | 2025-11-09 07:08:07.061Z | 281.523° WNW | 41.881° | 2025-11-09 07:14:07.061Z | 352.246° N |
| 12 mins | 2025-11-09 18:12:07.061Z | 9.652° NNE | 2025-11-09 18:17:07.061Z | 67.919° E | 41.437° | 2025-11-09 18:24:07.061Z | 169.575° S |
| 5 mins | 2025-11-09 20:00:07.061Z | 321.251° NNW | 2025-11-09 20:03:07.061Z | 290.12° WNW | 19.268° | 2025-11-09 20:05:07.061Z | 266.731° W |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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