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 23150.44794607 .00000267 00000-0 12574-3 0 9992
2 27597 98.6479 94.9063 0002207 82.1346 278.0085 14.27908907 65481
| Epoch (UTC): | 30 May 2023 10:45:02 |
| Eccentricity: | 0.0002207 |
| inclination: | 98.6479° |
| perigee height: | 797 km |
| apogee height: | 800 km |
| right ascension of ascending node: | 94.9063° |
| argument of perigee: | 82.1346° |
| revolutions per day: | 14.27908907 |
| mean anomaly at epoch: | 278.0085° |
| orbit number at epoch: | 6548 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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