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 55586U 26144.88673698 +.00000000 +00000-0 -19405-3 0 00007
2 55586 42.9992 295.1008 0001354 306.2892 53.7835 15.27618245 06
| Epoch (UTC): | 24 May 2026 21:16:54 |
| Eccentricity: | 0.0001354 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 295.1008° |
| argument of perigee: | 306.2892° |
| revolutions per day: | 15.27618245 |
| mean anomaly at epoch: | 53.7835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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