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 39059U 13001C 23083.75695675 .00000044 00000-0 24555-3 0 9999
2 39059 82.4997 235.8198 0027056 89.6729 270.7447 12.42874281462129
| Epoch (UTC): | 24 March 2023 18:10:01 |
| Eccentricity: | 0.0027056 |
| inclination: | 82.4997° |
| perigee height: | 1473 km |
| apogee height: | 1516 km |
| right ascension of ascending node: | 235.8198° |
| argument of perigee: | 89.6729° |
| revolutions per day: | 12.42874281 |
| mean anomaly at epoch: | 270.7447° |
| orbit number at epoch: | 46212 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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