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 59588U 26073.53783455 +.00000000 +00000-0 +27219-1 0 00008
2 59588 97.2039 13.5597 0064161 64.9868 295.7941 13.89866956 04
| Epoch (UTC): | 14 March 2026 12:54:28 |
| Eccentricity: | 0.0064161 |
| inclination: | 97.2039° |
| perigee height: | 882 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 13.5597° |
| argument of perigee: | 64.9868° |
| revolutions per day: | 13.89866956 |
| mean anomaly at epoch: | 295.7941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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