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 43495U 18052A 22239.97056714 0.00000000 00000-0 00000-0 0 01
2 43495 97.3711 355.0194 0000744 190.8766 169.1232 15.25981692 06
| Epoch (UTC): | 27 August 2022 23:17:37 |
| Eccentricity: | 0.0000744 |
| inclination: | 97.3711° |
| perigee height: | 487 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 355.0194° |
| argument of perigee: | 190.8766° |
| revolutions per day: | 15.25981692 |
| mean anomaly at epoch: | 169.1232° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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