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 68818U 26145.29896117 +.00000000 +00000-0 +13423-2 0 00000
2 68818 97.2863 351.9693 0001961 77.4845 282.6639 15.75242816 03
| Epoch (UTC): | 25 May 2026 07:10:30 |
| Eccentricity: | 0.0001961 |
| inclination: | 97.2863° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9693° |
| argument of perigee: | 77.4845° |
| revolutions per day: | 15.75242816 |
| mean anomaly at epoch: | 282.6639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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