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 54600U 22151NA 24358.06383658 .00020479 00000-0 44983-2 0 9999
2 54600 98.6474 25.3690 0090127 158.4069 202.0966 14.55042295111029
| Epoch (UTC): | 23 December 2024 01:31:55 |
| Eccentricity: | 0.0090127 |
| inclination: | 98.6474° |
| perigee height: | 645 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 25.3690° |
| argument of perigee: | 158.4069° |
| revolutions per day: | 14.55042295 |
| mean anomaly at epoch: | 202.0966° |
| orbit number at epoch: | 11102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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