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 43676U 18084F 24263.49012330 .00006328 00000-0 57073-3 0 9990
2 43676 98.0541 51.5784 0014395 58.7943 301.4686 14.95832600320521
| Epoch (UTC): | 19 September 2024 11:45:46 |
| Eccentricity: | 0.0014395 |
| inclination: | 98.0541° |
| perigee height: | 570 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 51.5784° |
| argument of perigee: | 58.7943° |
| revolutions per day: | 14.95832600 |
| mean anomaly at epoch: | 301.4686° |
| orbit number at epoch: | 32052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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