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 24286.77737239 -.00000020 00000-0 65136-3 0 9997
2 00053 47.2768 71.3690 0099552 66.6822 294.4406 12.17351755860820
| Epoch (UTC): | 12 October 2024 18:39:24 |
| Eccentricity: | 0.0099552 |
| inclination: | 47.2768° |
| perigee height: | 1524 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 71.3690° |
| argument of perigee: | 66.6822° |
| revolutions per day: | 12.17351755 |
| mean anomaly at epoch: | 294.4406° |
| orbit number at epoch: | 86082 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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