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 55291U 26145.58285757 +.00000000 +00000-0 -64766-4 0 00004
2 55291 69.9994 190.7142 0003589 269.1535 90.9213 14.98322510 09
| Epoch (UTC): | 25 May 2026 13:59:18 |
| Eccentricity: | 0.0003589 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 190.7142° |
| argument of perigee: | 269.1535° |
| revolutions per day: | 14.98322510 |
| mean anomaly at epoch: | 90.9213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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