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 00559U 26108.23743252 +.00000000 +00000-0 +67599-3 0 00006
2 00559 66.5962 100.2629 0044414 213.2142 146.6189 14.72722358 03
| Epoch (UTC): | 18 April 2026 05:41:54 |
| Eccentricity: | 0.0044414 |
| inclination: | 66.5962° |
| perigee height: | 621 km |
| apogee height: | 684 km |
| right ascension of ascending node: | 100.2629° |
| argument of perigee: | 213.2142° |
| revolutions per day: | 14.72722358 |
| mean anomaly at epoch: | 146.6189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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