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 55404U 26145.33714360 +.00000000 +00000-0 -84741-4 0 00005
2 55404 69.9996 231.3111 0003166 270.5338 89.5458 14.98322418 05
| Epoch (UTC): | 25 May 2026 08:05:29 |
| Eccentricity: | 0.0003166 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 231.3111° |
| argument of perigee: | 270.5338° |
| revolutions per day: | 14.98322418 |
| mean anomaly at epoch: | 89.5458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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