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 23269.91493802 .00000293 00000-0 10985-3 0 9995
2 27386 98.2434 235.7978 0001216 87.6846 332.5285 14.38412276130581
| Epoch (UTC): | 26 September 2023 21:57:30 |
| Eccentricity: | 0.0001216 |
| inclination: | 98.2434° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 235.7978° |
| argument of perigee: | 87.6846° |
| revolutions per day: | 14.38412276 |
| mean anomaly at epoch: | 332.5285° |
| orbit number at epoch: | 13058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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