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 65559U 26145.38753197 +.00000000 +00000-0 +18668-3 0 00006
2 65559 49.9814 144.5849 0007585 200.6718 159.3915 14.84091529 07
| Epoch (UTC): | 25 May 2026 09:18:02 |
| Eccentricity: | 0.0007585 |
| inclination: | 49.9814° |
| perigee height: | 611 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 144.5849° |
| argument of perigee: | 200.6718° |
| revolutions per day: | 14.84091529 |
| mean anomaly at epoch: | 159.3915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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