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 42065U 17011B 23066.76701012 0.00000000 00000-0 00000-0 0 01
2 42065 63.4423 320.5038 0061385 4.5330 355.4669 13.40859630 07
| Epoch (UTC): | 07 March 2023 18:24:29 |
| Eccentricity: | 0.0061385 |
| inclination: | 63.4423° |
| perigee height: | 1060 km |
| apogee height: | 1152 km |
| right ascension of ascending node: | 320.5038° |
| argument of perigee: | 4.5330° |
| revolutions per day: | 13.40859630 |
| mean anomaly at epoch: | 355.4669° |
| 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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