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 60553U 24149CP 24358.17099703 .00002682 00000-0 25445-3 0 9998
2 60553 97.7333 71.7210 0009857 94.6462 265.5885 14.94345298 19155
| Epoch (UTC): | 23 December 2024 04:06:14 |
| Eccentricity: | 0.0009857 |
| inclination: | 97.7333° |
| perigee height: | 577 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 71.7210° |
| argument of perigee: | 94.6462° |
| revolutions per day: | 14.94345298 |
| mean anomaly at epoch: | 265.5885° |
| orbit number at epoch: | 1915 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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