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: 9 hours ago
TLE from 9 hours ago
0 QIANFAN-49
1 62250U 24232P 26246.83774078 .00000087 00000-0 11659-3 0 9992
2 62250 89.0142 14.6216 0015555 144.1468 216.0731 13.51028087103638Epoch: 2026-09-03T20:06Z
TLE epoch observation values (Epoch: 2026-09-03T20:06:20.803Z)
Latitude
0.00005°
Longitude
90.06474°
Altitude
1,080.802 km
Speed
7.307 km/s
True Right ascension
00h 58m 29s
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
21:06:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,077.108 km
Perigee altitude
1,053.951 km
Semi-major axis
7,443.666 km
Eccentricity
0.00156
Inclination
89.0142°
RAAN
14.6216°
Arg. of periapsis
144.1468°
True anomaly
215.96831°
Mean anomaly
216.0731°
Eccentric anomaly
216.02069°
Mean motion
3.37958 °/min
Orbital period
106.52 mins
BSTAR
0.00011659
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-09-04 08:38:19.399Z | 162.414° S | 2026-09-04 08:44:19.399Z | 103.77° ESE | 40.75° | 2026-09-04 08:50:19.399Z | 8.236° NNE |
| 8 mins | 2026-09-04 10:28:19.399Z | 244.819° WSW | 2026-09-04 10:31:19.399Z | 276.399° WNW | 19.611° | 2026-09-04 10:36:19.399Z | 327.296° NNW |
| 9 mins | 2026-09-04 19:50:19.399Z | 35.393° NE | 2026-09-04 19:54:19.399Z | 86.432° E | 25.61° | 2026-09-04 19:59:19.399Z | 138.29° SSE |
| 10 mins | 2026-09-04 21:36:19.399Z | 340.128° N | 2026-09-04 21:40:19.399Z | 286.511° WNW | 34.521° | 2026-09-04 21:46:19.399Z | 210.976° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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