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 63191U 26145.24994338 +.00000000 +00000-0 +15472-2 0 00004
2 63191 43.0031 218.2749 0005447 286.4105 73.6164 15.70989108 07
| Epoch (UTC): | 25 May 2026 05:59:55 |
| Eccentricity: | 0.0005447 |
| inclination: | 43.0031° |
| perigee height: | 352 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 218.2749° |
| argument of perigee: | 286.4105° |
| revolutions per day: | 15.70989108 |
| mean anomaly at epoch: | 73.6164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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