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 59125U 26145.32582796 +.00000000 +00000-0 +21820-3 0 00001
2 59125 97.5607 285.7112 0008067 320.2422 39.8229 15.35636519 07
| Epoch (UTC): | 25 May 2026 07:49:11 |
| Eccentricity: | 0.0008067 |
| inclination: | 97.5607° |
| perigee height: | 454 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 285.7112° |
| argument of perigee: | 320.2422° |
| revolutions per day: | 15.35636519 |
| mean anomaly at epoch: | 39.8229° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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