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 59841U 26145.56812525 +.00000000 +00000-0 +23693-3 0 00008
2 59841 43.0014 192.4654 0000823 278.3175 81.7583 15.27552133 04
| Epoch (UTC): | 25 May 2026 13:38:06 |
| Eccentricity: | 0.0000823 |
| inclination: | 43.0014° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 192.4654° |
| argument of perigee: | 278.3175° |
| revolutions per day: | 15.27552133 |
| mean anomaly at epoch: | 81.7583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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