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 55276U 26145.57867884 +.00000000 +00000-0 -18944-3 0 00009
2 55276 69.9991 190.7019 0003898 268.1738 91.8975 14.98330972 05
| Epoch (UTC): | 25 May 2026 13:53:17 |
| Eccentricity: | 0.0003898 |
| inclination: | 69.9991° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.7019° |
| argument of perigee: | 268.1738° |
| revolutions per day: | 14.98330972 |
| mean anomaly at epoch: | 91.8975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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