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 59155U 26145.39537594 +.00000000 +00000-0 +40286-4 0 00005
2 59155 42.9996 37.5458 0000762 284.5512 75.5255 15.27585420 08
| Epoch (UTC): | 25 May 2026 09:29:20 |
| Eccentricity: | 0.0000762 |
| inclination: | 42.9996° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 37.5458° |
| argument of perigee: | 284.5512° |
| revolutions per day: | 15.27585420 |
| mean anomaly at epoch: | 75.5255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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