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 54191U 26145.32365278 +.00000000 +00000-0 -12906-3 0 00009
2 54191 53.2155 10.3326 0001454 83.5290 276.5867 15.08830645 00
| Epoch (UTC): | 25 May 2026 07:46:03 |
| Eccentricity: | 0.0001454 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 10.3326° |
| argument of perigee: | 83.5290° |
| revolutions per day: | 15.08830645 |
| mean anomaly at epoch: | 276.5867° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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