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 40376U 15003A 24284.51548573 .00002862 00000-0 56302-3 0 9994
2 40376 98.1313 289.2879 0001260 95.0669 265.0677 14.63348748517729
| Epoch (UTC): | 10 October 2024 12:22:17 |
| Eccentricity: | 0.0001260 |
| inclination: | 98.1313° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 289.2879° |
| argument of perigee: | 95.0669° |
| revolutions per day: | 14.63348748 |
| mean anomaly at epoch: | 265.0677° |
| orbit number at epoch: | 51772 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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