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 41918U 17003B 23149.87956311 .00000251 00000-0 82700-4 0 9992
2 41918 86.4010 194.0717 0002665 88.3836 271.7665 14.34219158333515
| Epoch (UTC): | 29 May 2023 21:06:34 |
| Eccentricity: | 0.0002665 |
| inclination: | 86.4010° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 194.0717° |
| argument of perigee: | 88.3836° |
| revolutions per day: | 14.34219158 |
| mean anomaly at epoch: | 271.7665° |
| orbit number at epoch: | 33351 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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