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 27432U 02024C 23151.57722875 .00000060 00000-0 54966-4 0 9991
2 27432 99.0236 185.9798 0050561 14.6493 138.4797 14.14214012 86025
| Epoch (UTC): | 31 May 2023 13:51:12 |
| Eccentricity: | 0.0050561 |
| inclination: | 99.0236° |
| perigee height: | 808 km |
| apogee height: | 881 km |
| right ascension of ascending node: | 185.9798° |
| argument of perigee: | 14.6493° |
| revolutions per day: | 14.14214012 |
| mean anomaly at epoch: | 138.4797° |
| orbit number at epoch: | 8602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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