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 59375U 26145.61783119 +.00000000 +00000-0 +79887-4 0 00009
2 59375 53.1613 260.8855 0001313 103.3423 256.7726 15.34386932 07
| Epoch (UTC): | 25 May 2026 14:49:40 |
| Eccentricity: | 0.0001313 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 260.8855° |
| argument of perigee: | 103.3423° |
| revolutions per day: | 15.34386932 |
| mean anomaly at epoch: | 256.7726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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