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 42679U 16049D 24280.83280229 .00001367 00000-0 39475-3 0 9996
2 42679 98.3376 291.9682 0008001 79.0199 281.1892 14.46106185430449
| Epoch (UTC): | 06 October 2024 19:59:14 |
| Eccentricity: | 0.0008001 |
| inclination: | 98.3376° |
| perigee height: | 733 km |
| apogee height: | 744 km |
| right ascension of ascending node: | 291.9682° |
| argument of perigee: | 79.0199° |
| revolutions per day: | 14.46106185 |
| mean anomaly at epoch: | 281.1892° |
| orbit number at epoch: | 43044 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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