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 63179U 26145.38748166 +.00000000 +00000-0 +78772-4 0 00005
2 63179 97.9585 331.1231 0007679 247.8631 112.1763 14.74319387 03
| Epoch (UTC): | 25 May 2026 09:17:58 |
| Eccentricity: | 0.0007679 |
| inclination: | 97.9585° |
| perigee height: | 642 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 331.1231° |
| argument of perigee: | 247.8631° |
| revolutions per day: | 14.74319387 |
| mean anomaly at epoch: | 112.1763° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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