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 55161U 26145.40177684 +.00000000 +00000-0 -43831-3 0 00009
2 55161 87.8909 25.6110 0001589 88.5557 271.5753 13.11418722 07
| Epoch (UTC): | 25 May 2026 09:38:33 |
| Eccentricity: | 0.0001589 |
| inclination: | 87.8909° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6110° |
| argument of perigee: | 88.5557° |
| revolutions per day: | 13.11418722 |
| mean anomaly at epoch: | 271.5753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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