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 68518U 26145.37258781 +.00000000 +00000-0 +52314-3 0 00008
2 68518 53.1598 131.7932 0001019 72.9713 287.1401 15.34401976 00
| Epoch (UTC): | 25 May 2026 08:56:31 |
| Eccentricity: | 0.0001019 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 131.7932° |
| argument of perigee: | 72.9713° |
| revolutions per day: | 15.34401976 |
| mean anomaly at epoch: | 287.1401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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