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 63058U 26144.78008192 +.00000000 +00000-0 +11826-2 0 00007
2 63058 43.0005 277.0757 0002829 247.2685 112.7884 15.70842292 07
| Epoch (UTC): | 24 May 2026 18:43:19 |
| Eccentricity: | 0.0002829 |
| inclination: | 43.0005° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 277.0757° |
| argument of perigee: | 247.2685° |
| revolutions per day: | 15.70842292 |
| mean anomaly at epoch: | 112.7884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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