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 52475U 26145.49983858 +.00000000 +00000-0 +75396-4 0 00002
2 52475 53.2133 74.5279 0001667 69.3780 290.7391 15.08833046 08
| Epoch (UTC): | 25 May 2026 11:59:46 |
| Eccentricity: | 0.0001667 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 74.5279° |
| argument of perigee: | 69.3780° |
| revolutions per day: | 15.08833046 |
| mean anomaly at epoch: | 290.7391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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