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 27386U 02009A 24260.64474794 .00000578 00000-0 20225-3 0 9990
2 27386 98.2926 218.5993 0001259 89.7174 83.3676 14.38675504181651
| Epoch (UTC): | 16 September 2024 15:28:26 |
| Eccentricity: | 0.0001259 |
| inclination: | 98.2926° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 218.5993° |
| argument of perigee: | 89.7174° |
| revolutions per day: | 14.38675504 |
| mean anomaly at epoch: | 83.3676° |
| orbit number at epoch: | 18165 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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