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 51462U 26145.40692791 +.00000000 +00000-0 -86738-6 0 00006
2 51462 53.2131 294.7326 0001479 91.5610 268.5552 15.08839145 08
| Epoch (UTC): | 25 May 2026 09:45:58 |
| Eccentricity: | 0.0001479 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 294.7326° |
| argument of perigee: | 91.5610° |
| revolutions per day: | 15.08839145 |
| mean anomaly at epoch: | 268.5552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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