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 42759U 17034B 25117.58805814 .00081204 00000-0 10479-2 0 9995
2 42759 43.0087 217.0929 0019531 347.0370 12.9989 15.57800626435880
| Epoch (UTC): | 27 April 2025 14:06:48 |
| Eccentricity: | 0.0019531 |
| inclination: | 43.0087° |
| perigee height: | 381 km |
| apogee height: | 407 km |
| right ascension of ascending node: | 217.0929° |
| argument of perigee: | 347.0370° |
| revolutions per day: | 15.57800626 |
| mean anomaly at epoch: | 12.9989° |
| orbit number at epoch: | 43588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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