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 46055U 26145.19053698 +.00000000 +00000-0 +34746-4 0 00000
2 46055 53.1598 118.2267 0001068 85.5676 274.5447 15.31697810 06
| Epoch (UTC): | 25 May 2026 04:34:22 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 118.2267° |
| argument of perigee: | 85.5676° |
| revolutions per day: | 15.31697810 |
| mean anomaly at epoch: | 274.5447° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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