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 60193U 26145.41608412 +.00000000 +00000-0 +11401-4 0 00007
2 60193 53.1588 143.1070 0001214 66.2035 293.9110 15.69706249 01
| Epoch (UTC): | 25 May 2026 09:59:09 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 143.1070° |
| argument of perigee: | 66.2035° |
| revolutions per day: | 15.69706249 |
| mean anomaly at epoch: | 293.9110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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