QIANFAN-47, 62248
Orbit data source: Space-Track
QIANFAN-47, 62248 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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62248 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: 7 hours ago
TLE from 7 hours ago
0 QIANFAN-47
1 62248U 24232M 25287.93429368 .00000145 00000-0 20630-3 0 9997
2 62248 89.0020 47.1432 0014808 14.9651 345.1935 13.50978790 91303Epoch: 2025-10-14T22:25Z
TLE epoch observation values (Epoch: 2025-10-14T22:25:22.973Z)
Latitude
-0.00009°
Longitude
47.08188°
Altitude
1,060.951 km
Speed
7.327 km/s
True Right ascension
03h 08m 34s
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
00:15:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,076.733 km
Perigee altitude
1,054.688 km
Semi-major axis
7,443.848 km
Eccentricity
0.00148
Inclination
89.002°
RAAN
47.1432°
Arg. of periapsis
14.9651°
True anomaly
345.15006°
Mean anomaly
345.1935°
Eccentric anomaly
345.17179°
Mean motion
3.37946 °/min
Orbital period
106.53 mins
BSTAR
0.0002063
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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-47 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 07:26:01.448Z | 130.856° SE | 2025-10-15 07:31:01.448Z | 75.047° E | 25.79° | 2025-10-15 07:36:01.448Z | 22.545° NE |
| 11 mins | 2025-10-15 09:12:01.448Z | 208.164° SW | 2025-10-15 09:17:01.448Z | 272.496° WNW | 34.692° | 2025-10-15 09:23:01.448Z | 344.862° N |
| 4 mins | 2025-10-15 18:38:01.448Z | 62.537° ENE | 2025-10-15 18:39:01.448Z | 72.118° E | 12.931° | 2025-10-15 18:42:01.448Z | 99.68° ESE |
| 12 mins | 2025-10-15 20:21:01.448Z | 1.043° NNE | 2025-10-15 20:27:01.448Z | 180.059° SSW | 44.63° | 2025-10-15 20:33:01.448Z | 182.691° SSW |
| 4 mins | 2025-10-15 22:11:01.448Z | 300.598° NW | 2025-10-15 22:12:01.448Z | 290.889° WNW | 13.35° | 2025-10-15 22:15:01.448Z | 263.239° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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