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 58830U 26145.44074616 +.00000000 +00000-0 +38986-4 0 00005
2 58830 53.1597 207.3601 0001188 87.7512 272.3625 15.31699696 05
| Epoch (UTC): | 25 May 2026 10:34:40 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1597° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 207.3601° |
| argument of perigee: | 87.7512° |
| revolutions per day: | 15.31699696 |
| mean anomaly at epoch: | 272.3625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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