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: 15 hours ago
TLE from 15 hours ago
0 QIANFAN-49
1 62250U 24232P 25287.95897948 .00000162 00000-0 23287-3 0 9995
2 62250 89.0020 47.1533 0014041 12.4170 347.7324 13.50978780 59905Epoch: 2025-10-14T23:00Z
TLE epoch observation values (Epoch: 2025-10-14T23:00:55.827Z)
Latitude
-0.00004°
Longitude
38.18076°
Altitude
1,061.394 km
Speed
7.326 km/s
True Right ascension
03h 08m 36s
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
09:05:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.163 km
Perigee altitude
1,055.259 km
Semi-major axis
7,443.848 km
Eccentricity
0.0014
Inclination
89.002°
RAAN
47.1533°
Arg. of periapsis
12.417°
True anomaly
347.69815°
Mean anomaly
347.7324°
Eccentric anomaly
347.71528°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.00023287
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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 | 2025-10-15 19:10:28.634Z | 29.081° NE | 2025-10-15 19:15:28.634Z | 83.501° E | 23.736° | 2025-10-15 19:20:28.634Z | 134.055° SE |
| 10 mins | 2025-10-15 20:57:28.634Z | 343.663° N | 2025-10-15 21:02:28.634Z | 264.584° W | 36.88° | 2025-10-15 21:07:28.634Z | 207.772° SW |
| 8 mins | 2025-10-16 07:09:28.634Z | 114.913° SE | 2025-10-16 07:13:28.634Z | 70.104° E | 21.052° | 2025-10-16 07:17:28.634Z | 29.89° NE |
| 11 mins | 2025-10-16 08:54:28.634Z | 200.24° SSW | 2025-10-16 08:59:28.634Z | 286.03° WNW | 39.438° | 2025-10-16 09:05:28.634Z | 350.409° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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