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 61057U 26145.40877659 +.00000000 +00000-0 +17666-4 0 00006
2 61057 53.1598 293.4219 0000624 117.1334 242.9748 15.69709458 04
| Epoch (UTC): | 25 May 2026 09:48:38 |
| Eccentricity: | 0.0000624 |
| inclination: | 53.1598° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 293.4219° |
| argument of perigee: | 117.1334° |
| revolutions per day: | 15.69709458 |
| mean anomaly at epoch: | 242.9748° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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