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 59136U 26145.57132866 +.00000000 +00000-0 +15188-3 0 00009
2 59136 97.5579 283.0702 0008798 321.6400 38.4214 15.30212787 06
| Epoch (UTC): | 25 May 2026 13:42:42 |
| Eccentricity: | 0.0008798 |
| inclination: | 97.5579° |
| perigee height: | 469 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 283.0702° |
| argument of perigee: | 321.6400° |
| revolutions per day: | 15.30212787 |
| mean anomaly at epoch: | 38.4214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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