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 62579U 26145.46510074 +.00000000 +00000-0 +35869-4 0 00002
2 62579 54.9903 10.9171 0012985 55.5371 304.6810 13.80606116 05
| Epoch (UTC): | 25 May 2026 11:09:44 |
| Eccentricity: | 0.0012985 |
| inclination: | 54.9903° |
| perigee height: | 952 km |
| apogee height: | 971 km |
| right ascension of ascending node: | 10.9171° |
| argument of perigee: | 55.5371° |
| revolutions per day: | 13.80606116 |
| mean anomaly at epoch: | 304.6810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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