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 59420U 26145.53172519 +.00000000 +00000-0 +40904-4 0 00005
2 59420 43.0031 342.5656 0000823 279.1729 80.9029 15.27573355 05
| Epoch (UTC): | 25 May 2026 12:45:41 |
| Eccentricity: | 0.0000823 |
| inclination: | 43.0031° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.5656° |
| argument of perigee: | 279.1729° |
| revolutions per day: | 15.27573355 |
| mean anomaly at epoch: | 80.9029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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