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 59791U 26145.43439488 +.00000000 +00000-0 +26412-4 0 00004
2 59791 43.0032 135.3852 0001570 273.1908 86.8764 15.27581234 02
| Epoch (UTC): | 25 May 2026 10:25:31 |
| Eccentricity: | 0.0001570 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.3852° |
| argument of perigee: | 273.1908° |
| revolutions per day: | 15.27581234 |
| mean anomaly at epoch: | 86.8764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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