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 68042U 26145.46920904 +.00000000 +00000-0 +38058-3 0 00002
2 68042 53.1609 53.2493 0001912 88.1855 271.9364 15.30203571 09
| Epoch (UTC): | 25 May 2026 11:15:39 |
| Eccentricity: | 0.0001912 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 53.2493° |
| argument of perigee: | 88.1855° |
| revolutions per day: | 15.30203571 |
| mean anomaly at epoch: | 271.9364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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