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 20478U 90013A 23154.69299973 -.00000068 00000-0 -16214-4 0 9997
2 20478 99.3723 189.5607 0004907 331.3159 28.7731 13.95667307617455
| Epoch (UTC): | 03 June 2023 16:37:55 |
| Eccentricity: | 0.0004907 |
| inclination: | 99.3723° |
| perigee height: | 905 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 189.5607° |
| argument of perigee: | 331.3159° |
| revolutions per day: | 13.95667307 |
| mean anomaly at epoch: | 28.7731° |
| orbit number at epoch: | 61745 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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