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 42075U 17016A 23080.75599137 -.00000113 00000-0 00000-0 0 9998
2 42075 0.0189 165.8543 0000070 275.1538 358.1310 1.00272422 22025
| Epoch (UTC): | 21 March 2023 18:08:37 |
| Eccentricity: | 0.0000070 |
| inclination: | 0.0189° |
| perigee height: | 35786 km |
| apogee height: | 35786 km |
| right ascension of ascending node: | 165.8543° |
| argument of perigee: | 275.1538° |
| revolutions per day: | 1.00272422 |
| mean anomaly at epoch: | 358.1310° |
| orbit number at epoch: | 2202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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