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 24357.86008330 .00000062 00000-0 14235-2 0 9995
2 00051 47.2134 284.3907 0109381 26.3280 334.3013 12.18348768865177
| Epoch (UTC): | 22 December 2024 20:38:31 |
| Eccentricity: | 0.0109381 |
| inclination: | 47.2134° |
| perigee height: | 1512 km |
| apogee height: | 1687 km |
| right ascension of ascending node: | 284.3907° |
| argument of perigee: | 26.3280° |
| revolutions per day: | 12.18348768 |
| mean anomaly at epoch: | 334.3013° |
| orbit number at epoch: | 86517 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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