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 68193U 26144.67394398 +.00000000 +00000-0 +56168-3 0 00005
2 68193 53.1602 273.3080 0000919 94.4347 265.6761 15.34399693 04
| Epoch (UTC): | 24 May 2026 16:10:28 |
| Eccentricity: | 0.0000919 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 273.3080° |
| argument of perigee: | 94.4347° |
| revolutions per day: | 15.34399693 |
| mean anomaly at epoch: | 265.6761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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