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 15595U 26159.46547596 +.00000000 +00000-0 +79389-4 0 00007
2 15595 108.0435 63.2987 0001255 281.6673 78.4328 14.39962331 02
| Epoch (UTC): | 08 June 2026 11:10:17 |
| Eccentricity: | 0.0001255 |
| inclination: | 108.0435° |
| perigee height: | 758 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 63.2987° |
| argument of perigee: | 281.6673° |
| revolutions per day: | 14.39962331 |
| mean anomaly at epoch: | 78.4328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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