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 58406U 26145.57957979 +.00000000 +00000-0 +24737-4 0 00009
2 58406 43.0018 338.4627 0001000 276.6061 83.4677 15.27576943 07
| Epoch (UTC): | 25 May 2026 13:54:35 |
| Eccentricity: | 0.0001000 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.4627° |
| argument of perigee: | 276.6061° |
| revolutions per day: | 15.27576943 |
| mean anomaly at epoch: | 83.4677° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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