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 40045U 14033AM 24357.43193815 .00009705 00000-0 10303-2 0 9999
2 40045 97.6769 164.2441 0046601 22.5724 337.7529 14.88433225565743
| Epoch (UTC): | 22 December 2024 10:21:59 |
| Eccentricity: | 0.0046601 |
| inclination: | 97.6769° |
| perigee height: | 570 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 164.2441° |
| argument of perigee: | 22.5724° |
| revolutions per day: | 14.88433225 |
| mean anomaly at epoch: | 337.7529° |
| orbit number at epoch: | 56574 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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