View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 26063U 00004C 24357.50734291 .00000401 00000-0 15219-3 0 9999
2 26063 100.2249 182.8177 0036461 124.8320 235.6299 14.37631525305440
| Epoch (UTC): | 22 December 2024 12:10:34 |
| Eccentricity: | 0.0036461 |
| inclination: | 100.2249° |
| perigee height: | 740 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 182.8177° |
| argument of perigee: | 124.8320° |
| revolutions per day: | 14.37631525 |
| mean anomaly at epoch: | 235.6299° |
| orbit number at epoch: | 30544 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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