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 59668U 26145.55233660 +.00000000 +00000-0 +53250-4 0 00004
2 59668 43.0019 320.3182 0001780 265.9511 94.1138 15.27578141 04
| Epoch (UTC): | 25 May 2026 13:15:21 |
| Eccentricity: | 0.0001780 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.3182° |
| argument of perigee: | 265.9511° |
| revolutions per day: | 15.27578141 |
| mean anomaly at epoch: | 94.1138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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