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 41519U 00055MT 24276.77327878 .00142933 00000-0 36790-1 0 9998
2 41519 98.8410 28.2679 0010760 156.5246 203.6439 14.49087398438464
| Epoch (UTC): | 02 October 2024 18:33:31 |
| Eccentricity: | 0.0010760 |
| inclination: | 98.8410° |
| perigee height: | 721 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 28.2679° |
| argument of perigee: | 156.5246° |
| revolutions per day: | 14.49087398 |
| mean anomaly at epoch: | 203.6439° |
| orbit number at epoch: | 43846 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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