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 00005U 26108.12683875 +.00000000 +00000-0 +19665-3 0 00005
2 00005 34.2498 139.6608 1836679 227.7068 115.2744 10.85971120 00
| Epoch (UTC): | 18 April 2026 03:02:38 |
| Eccentricity: | 0.1836679 |
| inclination: | 34.2498° |
| perigee height: | 654 km |
| apogee height: | 3818 km |
| right ascension of ascending node: | 139.6608° |
| argument of perigee: | 227.7068° |
| revolutions per day: | 10.85971120 |
| mean anomaly at epoch: | 115.2744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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