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 46174U 26145.39388469 +.00000000 +00000-0 +63401-3 0 00000
2 46174 53.0476 274.8755 0002061 208.8923 151.1974 15.56738229 04
| Epoch (UTC): | 25 May 2026 09:27:11 |
| Eccentricity: | 0.0002061 |
| inclination: | 53.0476° |
| perigee height: | 396 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 274.8755° |
| argument of perigee: | 208.8923° |
| revolutions per day: | 15.56738229 |
| mean anomaly at epoch: | 151.1974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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