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 23336.61062824 -.00000086 00000-0 00000-0 0 9994
2 42075 0.0124 340.6692 0000587 280.7760 17.5677 1.00270413 24598
| Epoch (UTC): | 02 December 2023 14:39:18 |
| Eccentricity: | 0.0000587 |
| inclination: | 0.0124° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 340.6692° |
| argument of perigee: | 280.7760° |
| revolutions per day: | 1.00270413 |
| mean anomaly at epoch: | 17.5677° |
| orbit number at epoch: | 2459 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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