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 30522U 99025AJL 24257.63376050 .00150699 00000-0 15030-1 0 9997
2 30522 99.3935 314.2829 0035548 112.3613 40.1951 14.90271629931210
| Epoch (UTC): | 13 September 2024 15:12:36 |
| Eccentricity: | 0.0035548 |
| inclination: | 99.3935° |
| perigee height: | 572 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 314.2829° |
| argument of perigee: | 112.3613° |
| revolutions per day: | 14.90271629 |
| mean anomaly at epoch: | 40.1951° |
| orbit number at epoch: | 93121 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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