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 03757U 68091AU 24280.65993564 .00037772 00000-0 59147-2 0 9993
2 03757 61.9875 19.7862 0393137 245.0175 110.9571 14.31890932744697
| Epoch (UTC): | 06 October 2024 15:50:18 |
| Eccentricity: | 0.0393137 |
| inclination: | 61.9875° |
| perigee height: | 504 km |
| apogee height: | 1067 km |
| right ascension of ascending node: | 19.7862° |
| argument of perigee: | 245.0175° |
| revolutions per day: | 14.31890932 |
| mean anomaly at epoch: | 110.9571° |
| orbit number at epoch: | 74469 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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