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 24282.58970027 .00000396 00000-0 46300-3 0 9994
2 04159 69.9629 58.1166 0115309 5.4541 354.7777 13.72736013753959
| Epoch (UTC): | 08 October 2024 14:09:10 |
| Eccentricity: | 0.0115309 |
| inclination: | 69.9629° |
| perigee height: | 905 km |
| apogee height: | 1075 km |
| right ascension of ascending node: | 58.1166° |
| argument of perigee: | 5.4541° |
| revolutions per day: | 13.72736013 |
| mean anomaly at epoch: | 354.7777° |
| orbit number at epoch: | 75395 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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