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 63583U 26145.57929956 +.00000000 +00000-0 +39255-3 0 00005
2 63583 42.9996 247.1168 0001341 269.9329 90.1369 15.27558863 02
| Epoch (UTC): | 25 May 2026 13:54:11 |
| Eccentricity: | 0.0001341 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.1168° |
| argument of perigee: | 269.9329° |
| revolutions per day: | 15.27558863 |
| mean anomaly at epoch: | 90.1369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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