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 68192U 26145.31267789 +.00000000 +00000-0 +67287-3 0 00003
2 68192 53.1581 270.1866 0001115 86.1279 273.9851 15.34411820 06
| Epoch (UTC): | 25 May 2026 07:30:15 |
| Eccentricity: | 0.0001115 |
| inclination: | 53.1581° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 270.1866° |
| argument of perigee: | 86.1279° |
| revolutions per day: | 15.34411820 |
| mean anomaly at epoch: | 273.9851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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