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 32794U 26145.58823513 +.00000000 +00000-0 +00000-0 0 00001
2 32794 0.3990 86.5308 0001260 55.5638 335.5525 1.00464942 07
| Epoch (UTC): | 25 May 2026 14:07:03 |
| Eccentricity: | 0.0001260 |
| inclination: | 0.3990° |
| perigee height: | 35727 km |
| apogee height: | 35738 km |
| right ascension of ascending node: | 86.5308° |
| argument of perigee: | 55.5638° |
| revolutions per day: | 1.00464942 |
| mean anomaly at epoch: | 335.5525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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