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 67092U 26145.38888272 +.00000000 +00000-0 +19597-3 0 00005
2 67092 70.0012 181.1702 0003700 267.1919 92.8817 14.98333396 05
| Epoch (UTC): | 25 May 2026 09:19:59 |
| Eccentricity: | 0.0003700 |
| inclination: | 70.0012° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 181.1702° |
| argument of perigee: | 267.1919° |
| revolutions per day: | 14.98333396 |
| mean anomaly at epoch: | 92.8817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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