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 41923U 17003G 24287.20655682 .00001167 00000-0 40949-3 0 9991
2 41923 86.4005 344.1898 0002275 98.6555 261.4898 14.34217954405530
| Epoch (UTC): | 13 October 2024 04:57:26 |
| Eccentricity: | 0.0002275 |
| inclination: | 86.4005° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 344.1898° |
| argument of perigee: | 98.6555° |
| revolutions per day: | 14.34217954 |
| mean anomaly at epoch: | 261.4898° |
| orbit number at epoch: | 40553 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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