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 27608U 02058D 23088.63802505 .00002511 00000-0 34695-3 0 9997
2 27608 64.5564 51.0807 0057598 233.4339 126.1456 14.79232267 92602
| Epoch (UTC): | 29 March 2023 15:18:45 |
| Eccentricity: | 0.0057598 |
| inclination: | 64.5564° |
| perigee height: | 591 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 51.0807° |
| argument of perigee: | 233.4339° |
| revolutions per day: | 14.79232267 |
| mean anomaly at epoch: | 126.1456° |
| orbit number at epoch: | 9260 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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