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 20877U 90081AM 24357.58439531 .00031636 00000-0 41810-2 0 9996
2 20877 98.1855 13.0174 0013146 255.8618 219.9388 14.79842955789736
| Epoch (UTC): | 22 December 2024 14:01:31 |
| Eccentricity: | 0.0013146 |
| inclination: | 98.1855° |
| perigee height: | 620 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 13.0174° |
| argument of perigee: | 255.8618° |
| revolutions per day: | 14.79842955 |
| mean anomaly at epoch: | 219.9388° |
| orbit number at epoch: | 78973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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