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 59905U 26145.43381353 +.00000000 +00000-0 -50287-5 0 00007
2 59905 43.0027 48.5507 0000708 269.7657 90.3113 15.27580733 00
| Epoch (UTC): | 25 May 2026 10:24:41 |
| Eccentricity: | 0.0000708 |
| inclination: | 43.0027° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 48.5507° |
| argument of perigee: | 269.7657° |
| revolutions per day: | 15.27580733 |
| mean anomaly at epoch: | 90.3113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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