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 55166U 26145.60687150 +.00000000 +00000-0 -42040-4 0 00002
2 55166 87.9152 10.3652 0001831 79.2370 280.8968 13.17649097 03
| Epoch (UTC): | 25 May 2026 14:33:53 |
| Eccentricity: | 0.0001831 |
| inclination: | 87.9152° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.3652° |
| argument of perigee: | 79.2370° |
| revolutions per day: | 13.17649097 |
| mean anomaly at epoch: | 280.8968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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