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 16615U 86019C 24284.14048052 .00001476 00000-0 55668-3 0 9998
2 16615 98.2678 315.6449 0012682 60.1717 344.5681 14.32735179 21886
| Epoch (UTC): | 10 October 2024 03:22:17 |
| Eccentricity: | 0.0012682 |
| inclination: | 98.2678° |
| perigee height: | 773 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 315.6449° |
| argument of perigee: | 60.1717° |
| revolutions per day: | 14.32735179 |
| mean anomaly at epoch: | 344.5681° |
| orbit number at epoch: | 2188 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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