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 55318U 26145.46995856 +.00000000 +00000-0 +45151-4 0 00005
2 55318 69.9986 170.8471 0003405 269.1124 90.9645 14.98332250 06
| Epoch (UTC): | 25 May 2026 11:16:44 |
| Eccentricity: | 0.0003405 |
| inclination: | 69.9986° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 170.8471° |
| argument of perigee: | 269.1124° |
| revolutions per day: | 14.98332250 |
| mean anomaly at epoch: | 90.9645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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