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 59355U 26145.46271399 +.00000000 +00000-0 +20819-4 0 00003
2 59355 43.0004 186.3365 0001471 271.4664 88.6019 15.27585479 00
| Epoch (UTC): | 25 May 2026 11:06:18 |
| Eccentricity: | 0.0001471 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.3365° |
| argument of perigee: | 271.4664° |
| revolutions per day: | 15.27585479 |
| mean anomaly at epoch: | 88.6019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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