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 55607U 26145.42526438 +.00000000 +00000-0 +14473-3 0 00000
2 55607 43.0031 280.9899 0001964 278.3051 81.7578 15.27558618 01
| Epoch (UTC): | 25 May 2026 10:12:22 |
| Eccentricity: | 0.0001964 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.9899° |
| argument of perigee: | 278.3051° |
| revolutions per day: | 15.27558618 |
| mean anomaly at epoch: | 81.7578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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