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 28649U 05017A 23155.86003427 .00001404 00000-0 16964-3 0 9996
2 28649 97.6674 209.0494 0002728 112.6843 247.4661 14.85241004979028
| Epoch (UTC): | 04 June 2023 20:38:26 |
| Eccentricity: | 0.0002728 |
| inclination: | 97.6674° |
| perigee height: | 611 km |
| apogee height: | 615 km |
| right ascension of ascending node: | 209.0494° |
| argument of perigee: | 112.6843° |
| revolutions per day: | 14.85241004 |
| mean anomaly at epoch: | 247.4661° |
| orbit number at epoch: | 97902 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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