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 59009U 26145.54673742 +.00000000 +00000-0 -91920-4 0 00008
2 59009 53.1607 80.9033 0001399 97.7664 262.3495 15.30199076 03
| Epoch (UTC): | 25 May 2026 13:07:18 |
| Eccentricity: | 0.0001399 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.9033° |
| argument of perigee: | 97.7664° |
| revolutions per day: | 15.30199076 |
| mean anomaly at epoch: | 262.3495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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