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 27597U 02056A 22222.79181541 .00000125 00000-0 68464-4 0 9999
2 27597 98.6083 165.8559 0000891 134.9004 225.2249 14.27631823 23721
| Epoch (UTC): | 10 August 2022 19:00:12 |
| Eccentricity: | 0.0000891 |
| inclination: | 98.6083° |
| perigee height: | 799 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 165.8559° |
| argument of perigee: | 134.9004° |
| revolutions per day: | 14.27631823 |
| mean anomaly at epoch: | 225.2249° |
| orbit number at epoch: | 2372 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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