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 58169U 26145.38863659 +.00000000 +00000-0 +30193-4 0 00008
2 58169 53.1607 223.2574 0000858 101.3485 258.7612 15.30192523 03
| Epoch (UTC): | 25 May 2026 09:19:38 |
| Eccentricity: | 0.0000858 |
| inclination: | 53.1607° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.2574° |
| argument of perigee: | 101.3485° |
| revolutions per day: | 15.30192523 |
| mean anomaly at epoch: | 258.7612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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