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 28647U 05016B 23151.77391481 .00005382 00000-0 28879-3 0 9996
2 28647 56.9936 165.3911 0107729 295.2514 63.7392 15.11650074222564
| Epoch (UTC): | 31 May 2023 18:34:26 |
| Eccentricity: | 0.0107729 |
| inclination: | 56.9936° |
| perigee height: | 457 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 165.3911° |
| argument of perigee: | 295.2514° |
| revolutions per day: | 15.11650074 |
| mean anomaly at epoch: | 63.7392° |
| orbit number at epoch: | 22256 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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