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 58790U 26145.26937654 +.00000000 +00000-0 +86138-4 0 00002
2 58790 43.0041 93.1294 0001232 272.8810 87.1901 15.27597377 06
| Epoch (UTC): | 25 May 2026 06:27:54 |
| Eccentricity: | 0.0001232 |
| inclination: | 43.0041° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.1294° |
| argument of perigee: | 272.8810° |
| revolutions per day: | 15.27597377 |
| mean anomaly at epoch: | 87.1901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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