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 55109U 26145.52029440 +.00000000 +00000-0 +35692-3 0 00005
2 55109 97.5566 238.3895 0003588 339.9106 20.1991 15.28034131 03
| Epoch (UTC): | 25 May 2026 12:29:13 |
| Eccentricity: | 0.0003588 |
| inclination: | 97.5566° |
| perigee height: | 479 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 238.3895° |
| argument of perigee: | 339.9106° |
| revolutions per day: | 15.28034131 |
| mean anomaly at epoch: | 20.1991° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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