QIANFAN-48, 62249
Orbit data source: Space-Track
QIANFAN-48, 62249 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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62249 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: 18 hours ago
TLE from 18 hours ago
0 QIANFAN-48
1 62249U 24232N 25322.41124631 .00000198 00000-0 28786-3 0 9994
2 62249 89.0048 43.6733 0015284 268.8569 91.0831 13.50988327 95961Epoch: 2025-11-18T09:52Z
TLE epoch observation values (Epoch: 2025-11-18T09:52:11.681Z)
Latitude
-0.00002°
Longitude
-162.07309°
Altitude
1,071.81 km
Speed
7.316 km/s
True Right ascension
02h 54m 41s
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
00:55:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.053 km
Perigee altitude
1,054.298 km
Semi-major axis
7,443.812 km
Eccentricity
0.00153
Inclination
89.0048°
RAAN
43.6733°
Arg. of periapsis
268.8569°
True anomaly
91.2582°
Mean anomaly
91.0831°
Eccentric anomaly
91.17065°
Mean motion
3.37948 °/min
Orbital period
106.53 mins
BSTAR
0.00028786
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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-48 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 | 2025-11-19 05:30:58.866Z | 159.903° S | 2025-11-19 05:36:58.866Z | 94.973° ESE | 39.941° | 2025-11-19 05:42:58.866Z | 9.17° NNE |
| 8 mins | 2025-11-19 07:20:58.866Z | 244.998° WSW | 2025-11-19 07:23:58.866Z | 278.42° WNW | 20.937° | 2025-11-19 07:28:58.866Z | 329.315° NNW |
| 9 mins | 2025-11-19 16:42:58.866Z | 36.956° NE | 2025-11-19 16:46:58.866Z | 86.597° E | 24.688° | 2025-11-19 16:51:58.866Z | 136.65° SSE |
| 10 mins | 2025-11-19 18:28:58.866Z | 341.334° N | 2025-11-19 18:32:58.866Z | 286.449° WNW | 35.983° | 2025-11-19 18:38:58.866Z | 208.944° SW |
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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