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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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-48
1 62249U 24232N 26246.85008754 .00000084 00000-0 11054-3 0 9999
2 62249 89.0143 14.6100 0018344 149.9221 210.2988 13.51020885135046Epoch: 2026-09-03T20:24Z
TLE epoch observation values (Epoch: 2026-09-03T20:24:07.563Z)
Latitude
0.00001°
Longitude
85.59614°
Altitude
1,083.261 km
Speed
7.305 km/s
True Right ascension
00h 58m 26s
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
20:52:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.21 km
Perigee altitude
1,051.901 km
Semi-major axis
7,443.693 km
Eccentricity
0.00183
Inclination
89.0143°
RAAN
14.61°
Arg. of periapsis
149.9221°
True anomaly
210.19296°
Mean anomaly
210.2988°
Eccentric anomaly
210.24586°
Mean motion
3.37956 °/min
Orbital period
106.52 mins
BSTAR
0.00011054
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-04 07:14:55.114Z | 88.969° E | 2026-09-04 07:16:55.114Z | 70.932° E | 11.838° | 2026-09-04 07:18:55.114Z | 52.622° ENE |
| 12 mins | 2026-09-04 08:56:55.114Z | 173.279° S | 2026-09-04 09:02:55.114Z | 34.334° NE | 44.371° | 2026-09-04 09:08:55.114Z | 0.979° NNE |
| 5 mins | 2026-09-04 10:47:55.114Z | 266.263° W | 2026-09-04 10:49:55.114Z | 286.117° WNW | 14.441° | 2026-09-04 10:52:55.114Z | 314.433° NW |
| 11 mins | 2026-09-04 20:06:55.114Z | 20.964° NNE | 2026-09-04 20:11:55.114Z | 84.265° E | 32.399° | 2026-09-04 20:17:55.114Z | 151.953° SSE |
| 9 mins | 2026-09-04 21:53:55.114Z | 334.264° NNW | 2026-09-04 21:57:55.114Z | 287.486° WNW | 27.761° | 2026-09-04 22:02:55.114Z | 226.826° WSW |
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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