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 59697U 26145.57734132 +.00000000 +00000-0 +22248-3 0 00000
2 59697 43.0010 345.4635 0001715 263.1941 96.8716 15.27576965 06
| Epoch (UTC): | 25 May 2026 13:51:22 |
| Eccentricity: | 0.0001715 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.4635° |
| argument of perigee: | 263.1941° |
| revolutions per day: | 15.27576965 |
| mean anomaly at epoch: | 96.8716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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