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 23031.52531824 .00000248 00000-0 95139-4 0 9991
2 27386 98.2129 7.2830 0001198 88.3397 22.1122 14.38232273 96310
| Epoch (UTC): | 31 January 2023 12:36:27 |
| Eccentricity: | 0.0001198 |
| inclination: | 98.2129° |
| perigee height: | 763 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 7.2830° |
| argument of perigee: | 88.3397° |
| revolutions per day: | 14.38232273 |
| mean anomaly at epoch: | 22.1122° |
| orbit number at epoch: | 9631 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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