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 58099U 26145.44485286 +.00000000 +00000-0 +25280-4 0 00004
2 58099 53.1597 158.9834 0001213 83.9006 276.2133 15.30194422 09
| Epoch (UTC): | 25 May 2026 10:40:35 |
| Eccentricity: | 0.0001213 |
| inclination: | 53.1597° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 158.9834° |
| argument of perigee: | 83.9006° |
| revolutions per day: | 15.30194422 |
| mean anomaly at epoch: | 276.2133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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