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 60548U 24149CJ 24358.21988019 .00011112 00000-0 10041-2 0 9997
2 60548 97.7344 71.8454 0006146 95.0422 265.1501 14.95619698 19162
| Epoch (UTC): | 23 December 2024 05:16:37 |
| Eccentricity: | 0.0006146 |
| inclination: | 97.7344° |
| perigee height: | 576 km |
| apogee height: | 585 km |
| right ascension of ascending node: | 71.8454° |
| argument of perigee: | 95.0422° |
| revolutions per day: | 14.95619698 |
| mean anomaly at epoch: | 265.1501° |
| orbit number at epoch: | 1916 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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