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 22027.51535555 .00000621 00000-0 67977-4 0 9993
2 00022 50.2823 216.5967 0137082 350.6480 9.1919 14.96095275558521
| Epoch (UTC): | 27 January 2022 12:22:06 |
| Eccentricity: | 0.0137082 |
| inclination: | 50.2823° |
| perigee height: | 483 km |
| apogee height: | 674 km |
| right ascension of ascending node: | 216.5967° |
| argument of perigee: | 350.6480° |
| revolutions per day: | 14.96095275 |
| mean anomaly at epoch: | 9.1919° |
| orbit number at epoch: | 55852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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