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 00046U 60007B 23088.67193645 .00001914 00000-0 40117-3 0 9996
2 00046 66.6904 182.1825 0199646 94.1142 268.2811 14.50332615286257
| Epoch (UTC): | 29 March 2023 16:07:35 |
| Eccentricity: | 0.0199646 |
| inclination: | 66.6904° |
| perigee height: | 583 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 182.1825° |
| argument of perigee: | 94.1142° |
| revolutions per day: | 14.50332615 |
| mean anomaly at epoch: | 268.2811° |
| orbit number at epoch: | 28625 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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