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 46356U 26145.58335647 +.00000000 +00000-0 +68393-3 0 00008
2 46356 53.0365 315.0332 0005527 223.5483 61.7391 15.82959940 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005527 |
| inclination: | 53.0365° |
| perigee height: | 318 km |
| apogee height: | 326 km |
| right ascension of ascending node: | 315.0332° |
| argument of perigee: | 223.5483° |
| revolutions per day: | 15.82959940 |
| mean anomaly at epoch: | 61.7391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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