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 59724U 26145.29493213 +.00000000 +00000-0 +39956-4 0 00007
2 59724 53.1606 143.8848 0001048 66.9255 293.1857 15.31705387 07
| Epoch (UTC): | 25 May 2026 07:04:42 |
| Eccentricity: | 0.0001048 |
| inclination: | 53.1606° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 143.8848° |
| argument of perigee: | 66.9255° |
| revolutions per day: | 15.31705387 |
| mean anomaly at epoch: | 293.1857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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