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 00022U 59009A 23080.51877855 .00006152 00000-0 43487-3 0 9999
2 00022 50.2815 48.1471 0128787 153.5569 207.2028 14.99661605621163
| Epoch (UTC): | 21 March 2023 12:27:02 |
| Eccentricity: | 0.0128787 |
| inclination: | 50.2815° |
| perigee height: | 478 km |
| apogee height: | 657 km |
| right ascension of ascending node: | 48.1471° |
| argument of perigee: | 153.5569° |
| revolutions per day: | 14.99661605 |
| mean anomaly at epoch: | 207.2028° |
| orbit number at epoch: | 62116 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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