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 43679U 18084J 24279.44597033 .00024663 00000-0 17460-2 0 9990
2 43679 98.0671 87.9462 0003566 101.6423 258.5202 15.04818676323834
| Epoch (UTC): | 05 October 2024 10:42:11 |
| Eccentricity: | 0.0003566 |
| inclination: | 98.0671° |
| perigee height: | 549 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 87.9462° |
| argument of perigee: | 101.6423° |
| revolutions per day: | 15.04818676 |
| mean anomaly at epoch: | 258.5202° |
| orbit number at epoch: | 32383 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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