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 55758U 26145.46856161 +.00000000 +00000-0 -31974-4 0 00007
2 55758 70.0004 50.7617 0002770 270.9311 89.1531 14.98331685 03
| Epoch (UTC): | 25 May 2026 11:14:43 |
| Eccentricity: | 0.0002770 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 50.7617° |
| argument of perigee: | 270.9311° |
| revolutions per day: | 14.98331685 |
| mean anomaly at epoch: | 89.1531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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