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 64055U 26145.64097336 +.00000000 +00000-0 +34975-3 0 00000
2 64055 42.0049 43.3119 0012829 198.2914 161.7452 15.01540349 06
| Epoch (UTC): | 25 May 2026 15:23:00 |
| Eccentricity: | 0.0012829 |
| inclination: | 42.0049° |
| perigee height: | 553 km |
| apogee height: | 571 km |
| right ascension of ascending node: | 43.3119° |
| argument of perigee: | 198.2914° |
| revolutions per day: | 15.01540349 |
| mean anomaly at epoch: | 161.7452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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