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 59613U 26145.56302016 +.00000000 +00000-0 +10257-4 0 00007
2 59613 43.0036 327.7010 0001928 282.7440 77.3196 15.27563793 00
| Epoch (UTC): | 25 May 2026 13:30:44 |
| Eccentricity: | 0.0001928 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.7010° |
| argument of perigee: | 282.7440° |
| revolutions per day: | 15.27563793 |
| mean anomaly at epoch: | 77.3196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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