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 59618U 26145.48348750 +.00000000 +00000-0 -16664-4 0 00007
2 59618 43.0024 327.9862 0000621 273.9720 86.1061 15.27570711 08
| Epoch (UTC): | 25 May 2026 11:36:13 |
| Eccentricity: | 0.0000621 |
| inclination: | 43.0024° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.9862° |
| argument of perigee: | 273.9720° |
| revolutions per day: | 15.27570711 |
| mean anomaly at epoch: | 86.1061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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