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 58073U 23159A 24358.16500507 .00000598 00000-0 23373-3 0 9992
2 58073 98.5502 21.5905 0000207 356.9273 3.1910 14.33183360 62329
| Epoch (UTC): | 23 December 2024 03:57:36 |
| Eccentricity: | 0.0000207 |
| inclination: | 98.5502° |
| perigee height: | 781 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 21.5905° |
| argument of perigee: | 356.9273° |
| revolutions per day: | 14.33183360 |
| mean anomaly at epoch: | 3.1910° |
| orbit number at epoch: | 6232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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