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 51898U 26145.63044998 +.00000000 +00000-0 -45859-4 0 00001
2 51898 53.2126 13.7209 0001602 89.3966 270.7210 15.08840643 02
| Epoch (UTC): | 25 May 2026 15:07:50 |
| Eccentricity: | 0.0001602 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 13.7209° |
| argument of perigee: | 89.3966° |
| revolutions per day: | 15.08840643 |
| mean anomaly at epoch: | 270.7210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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