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 59540U 26145.40359888 +.00000000 +00000-0 +20159-4 0 00000
2 59540 43.0025 270.5495 0001511 272.4828 87.5850 15.27578763 06
| Epoch (UTC): | 25 May 2026 09:41:10 |
| Eccentricity: | 0.0001511 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.5495° |
| argument of perigee: | 272.4828° |
| revolutions per day: | 15.27578763 |
| mean anomaly at epoch: | 87.5850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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