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 59545U 26145.40745375 +.00000000 +00000-0 +20705-4 0 00002
2 59545 43.0007 270.5751 0001344 265.6870 94.3828 15.27586299 05
| Epoch (UTC): | 25 May 2026 09:46:44 |
| Eccentricity: | 0.0001344 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.5751° |
| argument of perigee: | 265.6870° |
| revolutions per day: | 15.27586299 |
| mean anomaly at epoch: | 94.3828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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