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 28894U 05043E 23083.21938312 .00003115 00000-0 62480-3 0 9991
2 28894 98.1519 208.8183 0017241 25.9163 334.2899 14.62329796927989
| Epoch (UTC): | 24 March 2023 05:15:54 |
| Eccentricity: | 0.0017241 |
| inclination: | 98.1519° |
| perigee height: | 673 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 208.8183° |
| argument of perigee: | 25.9163° |
| revolutions per day: | 14.62329796 |
| mean anomaly at epoch: | 334.2899° |
| orbit number at epoch: | 92798 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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