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 58817U 26145.51867667 +.00000000 +00000-0 +49639-4 0 00001
2 58817 64.5131 146.7271 0009972 249.0286 110.9732 14.42704875 02
| Epoch (UTC): | 25 May 2026 12:26:53 |
| Eccentricity: | 0.0009972 |
| inclination: | 64.5131° |
| perigee height: | 742 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 146.7271° |
| argument of perigee: | 249.0286° |
| revolutions per day: | 14.42704875 |
| mean anomaly at epoch: | 110.9732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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