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 55306U 26145.36148323 +.00000000 +00000-0 +13327-4 0 00000
2 55306 69.9984 171.2725 0003368 269.6440 90.4333 14.98330478 01
| Epoch (UTC): | 25 May 2026 08:40:32 |
| Eccentricity: | 0.0003368 |
| inclination: | 69.9984° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 171.2725° |
| argument of perigee: | 269.6440° |
| revolutions per day: | 14.98330478 |
| mean anomaly at epoch: | 90.4333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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