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 55406U 26145.34131674 +.00000000 +00000-0 +10789-4 0 00009
2 55406 69.9995 231.3264 0003282 270.8351 89.2432 14.98329315 04
| Epoch (UTC): | 25 May 2026 08:11:29 |
| Eccentricity: | 0.0003282 |
| inclination: | 69.9995° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 231.3264° |
| argument of perigee: | 270.8351° |
| revolutions per day: | 14.98329315 |
| mean anomaly at epoch: | 89.2432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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