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 55597U 26145.39314277 +.00000000 +00000-0 +45856-5 0 00001
2 55597 43.0019 280.7580 0001448 269.9205 90.1481 15.27574480 06
| Epoch (UTC): | 25 May 2026 09:26:07 |
| Eccentricity: | 0.0001448 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 280.7580° |
| argument of perigee: | 269.9205° |
| revolutions per day: | 15.27574480 |
| mean anomaly at epoch: | 90.1481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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