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 59397U 26145.34238437 +.00000000 +00000-0 +76556-4 0 00001
2 59397 53.1597 259.8725 0001012 69.2951 290.8158 15.30201108 03
| Epoch (UTC): | 25 May 2026 08:13:02 |
| Eccentricity: | 0.0001012 |
| inclination: | 53.1597° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 259.8725° |
| argument of perigee: | 69.2951° |
| revolutions per day: | 15.30201108 |
| mean anomaly at epoch: | 290.8158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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