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 55942U 26145.59419669 +.00000000 +00000-0 +21465-4 0 00007
2 55942 69.9999 90.3968 0003341 261.5480 98.5301 14.98330830 05
| Epoch (UTC): | 25 May 2026 14:15:38 |
| Eccentricity: | 0.0003341 |
| inclination: | 69.9999° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 90.3968° |
| argument of perigee: | 261.5480° |
| revolutions per day: | 14.98330830 |
| mean anomaly at epoch: | 98.5301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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