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 53U 60009E 25082.90376666 .00000024 00000-0 10619-2 0 9998
2 53 47.2767 291.3025 0098263 184.1779 175.8197 12.17374612880570
| Epoch (UTC): | 23 March 2025 21:41:25 |
| Eccentricity: | 0.0098263 |
| inclination: | 47.2767° |
| perigee height: | 1525 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 291.3025° |
| argument of perigee: | 184.1779° |
| revolutions per day: | 12.17374612 |
| mean anomaly at epoch: | 175.8197° |
| orbit number at epoch: | 88057 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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