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 59806U 26145.63561902 +.00000000 +00000-0 +28992-3 0 00004
2 59806 97.3902 217.2311 0004951 189.8004 170.3134 15.16408171 09
| Epoch (UTC): | 25 May 2026 15:15:17 |
| Eccentricity: | 0.0004951 |
| inclination: | 97.3902° |
| perigee height: | 513 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 217.2311° |
| argument of perigee: | 189.8004° |
| revolutions per day: | 15.16408171 |
| mean anomaly at epoch: | 170.3134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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