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 55395U 26145.49150780 +.00000000 +00000-0 -29886-6 0 00002
2 55395 69.9994 230.6354 0003185 270.3146 89.7648 14.98332102 03
| Epoch (UTC): | 25 May 2026 11:47:46 |
| Eccentricity: | 0.0003185 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.6354° |
| argument of perigee: | 270.3146° |
| revolutions per day: | 14.98332102 |
| mean anomaly at epoch: | 89.7648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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