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 59205U 26145.45957030 +.00000000 +00000-0 +20295-4 0 00007
2 59205 53.1595 158.7292 0001078 72.5087 287.6032 15.30199379 05
| Epoch (UTC): | 25 May 2026 11:01:46 |
| Eccentricity: | 0.0001078 |
| inclination: | 53.1595° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 158.7292° |
| argument of perigee: | 72.5087° |
| revolutions per day: | 15.30199379 |
| mean anomaly at epoch: | 287.6032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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