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 59468U 26145.53348176 +.00000000 +00000-0 +28713-4 0 00005
2 59468 43.0037 316.3297 0002091 275.7946 84.2667 15.27576025 07
| Epoch (UTC): | 25 May 2026 12:48:12 |
| Eccentricity: | 0.0002091 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.3297° |
| argument of perigee: | 275.7946° |
| revolutions per day: | 15.27576025 |
| mean anomaly at epoch: | 84.2667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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