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 24283.82840896 .00000302 00000-0 36534-3 0 9997
2 04159 69.9629 55.5645 0115385 3.9213 356.2756 13.72736165754127
| Epoch (UTC): | 09 October 2024 19:52:54 |
| Eccentricity: | 0.0115385 |
| inclination: | 69.9629° |
| perigee height: | 905 km |
| apogee height: | 1075 km |
| right ascension of ascending node: | 55.5645° |
| argument of perigee: | 3.9213° |
| revolutions per day: | 13.72736165 |
| mean anomaly at epoch: | 356.2756° |
| orbit number at epoch: | 75412 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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