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 53U 60009E 23090.18416755 -.00000105 00000-0 -20687-3 0 9998
2 53 47.2800 3.4570 0097762 206.1893 153.3931 12.17292921792414
| Epoch (UTC): | 31 March 2023 04:25:12 |
| Eccentricity: | 0.0097762 |
| inclination: | 47.2800° |
| perigee height: | 1526 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 3.4570° |
| argument of perigee: | 206.1893° |
| revolutions per day: | 12.17292921 |
| mean anomaly at epoch: | 153.3931° |
| orbit number at epoch: | 79241 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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