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 23160.55414700 .00000054 00000-0 12143-4 0 9996
2 41918 86.3999 189.6169 0002498 84.8182 275.3299 14.34217023335042
| Epoch (UTC): | 09 June 2023 13:17:58 |
| Eccentricity: | 0.0002498 |
| inclination: | 86.3999° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 189.6169° |
| argument of perigee: | 84.8182° |
| revolutions per day: | 14.34217023 |
| mean anomaly at epoch: | 275.3299° |
| orbit number at epoch: | 33504 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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