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 59134U 26145.37235642 +.00000000 +00000-0 +35814-3 0 00009
2 59134 97.5545 290.3911 0006033 291.7576 68.3030 15.45365644 06
| Epoch (UTC): | 25 May 2026 08:56:11 |
| Eccentricity: | 0.0006033 |
| inclination: | 97.5545° |
| perigee height: | 426 km |
| apogee height: | 434 km |
| right ascension of ascending node: | 290.3911° |
| argument of perigee: | 291.7576° |
| revolutions per day: | 15.45365644 |
| mean anomaly at epoch: | 68.3030° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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