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 data is extracted from the following two-line orbital elements,
1 17590U 87027B 23152.55562196 -.00000190 00000-0 -70846-4 0 9999
2 17590 71.0035 248.7983 0006892 239.0026 121.0421 14.16886286872006
| Epoch (UTC): | 01 June 2023 13:20:05 |
| Eccentricity: | 0.0006892 |
| inclination: | 71.0035° |
| perigee height: | 831 km |
| apogee height: | 841 km |
| right ascension of ascending node: | 248.7983° |
| argument of perigee: | 239.0026° |
| revolutions per day: | 14.16886286 |
| mean anomaly at epoch: | 121.0421° |
| orbit number at epoch: | 87200 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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