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 23027.89669406 .00000348 00000-0 12825-3 0 9995
2 27386 98.2125 3.8127 0001187 88.3287 325.3608 14.38230049 95723
| Epoch (UTC): | 27 January 2023 21:31:14 |
| Eccentricity: | 0.0001187 |
| inclination: | 98.2125° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 3.8127° |
| argument of perigee: | 88.3287° |
| revolutions per day: | 14.38230049 |
| mean anomaly at epoch: | 325.3608° |
| orbit number at epoch: | 9572 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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