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 60919U 26145.65688921 +.00000000 +00000-0 -81065-6 0 00008
2 60919 53.1611 286.0078 0000997 79.1687 280.9426 15.30191902 00
| Epoch (UTC): | 25 May 2026 15:45:55 |
| Eccentricity: | 0.0000997 |
| inclination: | 53.1611° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.0078° |
| argument of perigee: | 79.1687° |
| revolutions per day: | 15.30191902 |
| mean anomaly at epoch: | 280.9426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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