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 23264.87911304 -.00000115 00000-0 -29048-3 0 9998
2 00053 47.2758 184.6759 0100797 1.8781 358.2369 12.17312321813698
| Epoch (UTC): | 21 September 2023 21:05:55 |
| Eccentricity: | 0.0100797 |
| inclination: | 47.2758° |
| perigee height: | 1524 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 184.6759° |
| argument of perigee: | 1.8781° |
| revolutions per day: | 12.17312321 |
| mean anomaly at epoch: | 358.2369° |
| orbit number at epoch: | 81369 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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