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 61193U 26145.57928578 +.00000000 +00000-0 +21802-3 0 00008
2 61193 97.5569 235.5837 0013376 14.9924 345.1698 15.08728749 02
| Epoch (UTC): | 25 May 2026 13:54:10 |
| Eccentricity: | 0.0013376 |
| inclination: | 97.5569° |
| perigee height: | 531 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 235.5837° |
| argument of perigee: | 14.9924° |
| revolutions per day: | 15.08728749 |
| mean anomaly at epoch: | 345.1698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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