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 41745U 16052B 23258.02975670 .00000105 00000-0 00000+0 0 9996
2 41745 1.5721 90.0154 0001688 133.6825 194.9467 1.00151814 17839
| Epoch (UTC): | 15 September 2023 00:42:50 |
| Eccentricity: | 0.0001688 |
| inclination: | 1.5721° |
| perigee height: | 35813 km |
| apogee height: | 35827 km |
| right ascension of ascending node: | 90.0154° |
| argument of perigee: | 133.6825° |
| revolutions per day: | 1.00151814 |
| mean anomaly at epoch: | 194.9467° |
| orbit number at epoch: | 1783 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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