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 24279.09974244 .00002082 00000-0 75002-3 0 9993
2 11416 98.6246 300.1838 0008933 298.4599 61.5685 14.34752216362223
| Epoch (UTC): | 05 October 2024 02:23:37 |
| Eccentricity: | 0.0008933 |
| inclination: | 98.6246° |
| perigee height: | 769 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 300.1838° |
| argument of perigee: | 298.4599° |
| revolutions per day: | 14.34752216 |
| mean anomaly at epoch: | 61.5685° |
| orbit number at epoch: | 36222 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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