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 11416U 79057A 24357.68997914 .00000605 00000-0 22823-3 0 9996
2 11416 98.6159 18.6141 0010947 65.7365 294.4963 14.34914511373280
| Epoch (UTC): | 22 December 2024 16:33:34 |
| Eccentricity: | 0.0010947 |
| inclination: | 98.6159° |
| perigee height: | 767 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 18.6141° |
| argument of perigee: | 65.7365° |
| revolutions per day: | 14.34914511 |
| mean anomaly at epoch: | 294.4963° |
| orbit number at epoch: | 37328 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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