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 55741U 26145.43936824 +.00000000 +00000-0 +14249-4 0 00006
2 55741 70.0009 51.0604 0002792 270.2626 89.8213 14.98331778 03
| Epoch (UTC): | 25 May 2026 10:32:41 |
| Eccentricity: | 0.0002792 |
| inclination: | 70.0009° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 51.0604° |
| argument of perigee: | 270.2626° |
| revolutions per day: | 14.98331778 |
| mean anomaly at epoch: | 89.8213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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