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 is defined by the following mean orbital elements,
1 58117U 26145.47009926 +.00000000 +00000-0 +53210-4 0 00005
2 58117 53.1597 169.1352 0001025 79.6232 280.4884 15.30191296 09
| Epoch (UTC): | 25 May 2026 11:16:56 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1597° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.1352° |
| argument of perigee: | 79.6232° |
| revolutions per day: | 15.30191296 |
| mean anomaly at epoch: | 280.4884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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