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 59855U 26145.49517133 +.00000000 +00000-0 +26218-3 0 00008
2 59855 42.9992 193.6281 0001331 275.5914 84.4785 15.27602728 06
| Epoch (UTC): | 25 May 2026 11:53:02 |
| Eccentricity: | 0.0001331 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.6281° |
| argument of perigee: | 275.5914° |
| revolutions per day: | 15.27602728 |
| mean anomaly at epoch: | 84.4785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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