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 55426U 26145.42917132 +.00000000 +00000-0 +29787-5 0 00000
2 55426 69.9992 251.1010 0003317 269.5632 90.5147 14.98329349 03
| Epoch (UTC): | 25 May 2026 10:18:00 |
| Eccentricity: | 0.0003317 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 251.1010° |
| argument of perigee: | 269.5632° |
| revolutions per day: | 14.98329349 |
| mean anomaly at epoch: | 90.5147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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