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 59635U 26145.49052549 +.00000000 +00000-0 +14365-5 0 00001
2 59635 43.0042 66.4219 0001060 273.2513 86.8217 15.27567587 06
| Epoch (UTC): | 25 May 2026 11:46:21 |
| Eccentricity: | 0.0001060 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 66.4219° |
| argument of perigee: | 273.2513° |
| revolutions per day: | 15.27567587 |
| mean anomaly at epoch: | 86.8217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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