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 58845U 26145.41351806 +.00000000 +00000-0 +44157-4 0 00004
2 58845 53.1605 297.5255 0001186 93.9108 266.2028 15.30190987 02
| Epoch (UTC): | 25 May 2026 09:55:27 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 297.5255° |
| argument of perigee: | 93.9108° |
| revolutions per day: | 15.30190987 |
| mean anomaly at epoch: | 266.2028° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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