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 61583U 26145.64508309 +.00000000 +00000-0 +16280-5 0 00001
2 61583 53.1593 277.1341 0000519 295.3108 64.7856 15.69693596 04
| Epoch (UTC): | 25 May 2026 15:28:55 |
| Eccentricity: | 0.0000519 |
| inclination: | 53.1593° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 277.1341° |
| argument of perigee: | 295.3108° |
| revolutions per day: | 15.69693596 |
| mean anomaly at epoch: | 64.7856° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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