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 58074U 23159B 24279.82301959 .00001013 00000-0 39692-3 0 9992
2 58074 98.4917 298.7899 0098707 313.9750 45.3322 14.28909452 50946
| Epoch (UTC): | 05 October 2024 19:45:08 |
| Eccentricity: | 0.0098707 |
| inclination: | 98.4917° |
| perigee height: | 724 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 298.7899° |
| argument of perigee: | 313.9750° |
| revolutions per day: | 14.28909452 |
| mean anomaly at epoch: | 45.3322° |
| orbit number at epoch: | 5094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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