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 22490U 93009B 23081.05807203 .00000631 00000-0 12476-3 0 9990
2 22490 24.9703 305.6310 0042629 227.4792 265.7728 14.44867617590142
| Epoch (UTC): | 22 March 2023 01:23:37 |
| Eccentricity: | 0.0042629 |
| inclination: | 24.9703° |
| perigee height: | 712 km |
| apogee height: | 773 km |
| right ascension of ascending node: | 305.6310° |
| argument of perigee: | 227.4792° |
| revolutions per day: | 14.44867617 |
| mean anomaly at epoch: | 265.7728° |
| orbit number at epoch: | 59014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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