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 40032U 14033Y 23275.78251952 .00008963 00000-0 84041-3 0 9994
2 40032 97.9743 217.8244 0008838 302.5220 57.5145 14.94221952504037
| Epoch (UTC): | 02 October 2023 18:46:49 |
| Eccentricity: | 0.0008838 |
| inclination: | 97.9743° |
| perigee height: | 578 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 217.8244° |
| argument of perigee: | 302.5220° |
| revolutions per day: | 14.94221952 |
| mean anomaly at epoch: | 57.5145° |
| orbit number at epoch: | 50403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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