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 55753U 26145.48125020 +.00000000 +00000-0 +10413-4 0 00001
2 55753 70.0007 50.8070 0002729 270.3170 89.7676 14.98330165 04
| Epoch (UTC): | 25 May 2026 11:33:00 |
| Eccentricity: | 0.0002729 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 50.8070° |
| argument of perigee: | 270.3170° |
| revolutions per day: | 14.98330165 |
| mean anomaly at epoch: | 89.7676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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