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 00053U 60009E 24277.82946706 .00000015 00000-0 98482-3 0 9997
2 00053 47.2751 98.9699 0099926 40.0866 320.7244 12.17349968859739
| Epoch (UTC): | 03 October 2024 19:54:25 |
| Eccentricity: | 0.0099926 |
| inclination: | 47.2751° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 98.9699° |
| argument of perigee: | 40.0866° |
| revolutions per day: | 12.17349968 |
| mean anomaly at epoch: | 320.7244° |
| orbit number at epoch: | 85973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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