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 68191U 26145.06055031 +.00000000 +00000-0 +88806-3 0 00009
2 68191 53.1578 271.4539 0001027 87.5326 272.5794 15.34417560 00
| Epoch (UTC): | 25 May 2026 01:27:11 |
| Eccentricity: | 0.0001027 |
| inclination: | 53.1578° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 271.4539° |
| argument of perigee: | 87.5326° |
| revolutions per day: | 15.34417560 |
| mean anomaly at epoch: | 272.5794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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