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 04159U 69082AB 24287.47166292 .00000219 00000-0 27894-3 0 9999
2 04159 69.9634 48.0597 0115585 359.4005 0.6930 13.72738413754623
| Epoch (UTC): | 13 October 2024 11:19:11 |
| Eccentricity: | 0.0115585 |
| inclination: | 69.9634° |
| perigee height: | 904 km |
| apogee height: | 1075 km |
| right ascension of ascending node: | 48.0597° |
| argument of perigee: | 359.4005° |
| revolutions per day: | 13.72738413 |
| mean anomaly at epoch: | 0.6930° |
| orbit number at epoch: | 75462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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