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 00051U 60009C 25073.55387316 -.00000128 00000-0 -42337-3 0 9991
2 00051 47.2155 31.6052 0109319 270.7663 88.0601 12.18356813875138
| Epoch (UTC): | 14 March 2025 13:17:34 |
| Eccentricity: | 0.0109319 |
| inclination: | 47.2155° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 31.6052° |
| argument of perigee: | 270.7663° |
| revolutions per day: | 12.18356813 |
| mean anomaly at epoch: | 88.0601° |
| orbit number at epoch: | 87513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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