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 27059U 01058E 23273.71391968 .00000051 00000-0 22792-3 0 9999
2 27059 82.5382 127.0179 0001844 358.0133 2.0949 12.61516496 1916
| Epoch (UTC): | 30 September 2023 17:08:02 |
| Eccentricity: | 0.0001844 |
| inclination: | 82.5382° |
| perigee height: | 1415 km |
| apogee height: | 1418 km |
| right ascension of ascending node: | 127.0179° |
| argument of perigee: | 358.0133° |
| revolutions per day: | 12.61516496 |
| mean anomaly at epoch: | 2.0949° |
| orbit number at epoch: | 191 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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