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 25286.97241530 .03437790 89859-5 10544-2 0 9999
2 42759 42.9888 273.3261 0008257 129.3938 230.7682 16.25684504462550
| Epoch (UTC): | 13 October 2025 23:20:16 |
| Eccentricity: | 0.0008257 |
| inclination: | 42.9888° |
| perigee height: | 199 km |
| apogee height: | 209 km |
| right ascension of ascending node: | 273.3261° |
| argument of perigee: | 129.3938° |
| revolutions per day: | 16.25684504 |
| mean anomaly at epoch: | 230.7682° |
| orbit number at epoch: | 46255 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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