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 20453U 90008B 24282.22214833 .00088740 00000-0 29218-2 0 9995
2 20453 35.6174 218.7767 0187968 289.0620 68.9832 15.15014309846649
| Epoch (UTC): | 08 October 2024 05:19:53 |
| Eccentricity: | 0.0187968 |
| inclination: | 35.6174° |
| perigee height: | 391 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 218.7767° |
| argument of perigee: | 289.0620° |
| revolutions per day: | 15.15014309 |
| mean anomaly at epoch: | 68.9832° |
| orbit number at epoch: | 84664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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