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 13563U 78026FA 24358.01982336 .00000887 00000-0 42064-3 0 9997
2 13563 98.8900 7.4466 0044200 71.3027 356.9192 14.21652514206274
| Epoch (UTC): | 23 December 2024 00:28:32 |
| Eccentricity: | 0.0044200 |
| inclination: | 98.8900° |
| perigee height: | 788 km |
| apogee height: | 851 km |
| right ascension of ascending node: | 7.4466° |
| argument of perigee: | 71.3027° |
| revolutions per day: | 14.21652514 |
| mean anomaly at epoch: | 356.9192° |
| orbit number at epoch: | 20627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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