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 59580U 26145.42466898 +.00000000 +00000-0 +67291-4 0 00004
2 59580 43.0005 295.1818 0001280 271.7042 88.3663 15.27578517 01
| Epoch (UTC): | 25 May 2026 10:11:31 |
| Eccentricity: | 0.0001280 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.1818° |
| argument of perigee: | 271.7042° |
| revolutions per day: | 15.27578517 |
| mean anomaly at epoch: | 88.3663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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