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 40105U 26145.11810404 +.00000000 +00000-0 +00000-0 0 00000
2 40105 55.3389 89.3836 0032426 118.5184 241.7812 2.00556877 02
| Epoch (UTC): | 25 May 2026 02:50:04 |
| Eccentricity: | 0.0032426 |
| inclination: | 55.3389° |
| perigee height: | 20097 km |
| apogee height: | 20269 km |
| right ascension of ascending node: | 89.3836° |
| argument of perigee: | 118.5184° |
| revolutions per day: | 2.00556877 |
| mean anomaly at epoch: | 241.7812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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