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 23031.47813245 .00000208 00000-0 12759-3 0 9996
2 17590 71.0037 143.8131 0003607 25.3695 334.7605 14.16856499854850
| Epoch (UTC): | 31 January 2023 11:28:30 |
| Eccentricity: | 0.0003607 |
| inclination: | 71.0037° |
| perigee height: | 833 km |
| apogee height: | 838 km |
| right ascension of ascending node: | 143.8131° |
| argument of perigee: | 25.3695° |
| revolutions per day: | 14.16856499 |
| mean anomaly at epoch: | 334.7605° |
| orbit number at epoch: | 85485 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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