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 25196.94858571 -.00000071 00000-0 -11670-4 0 9995
2 17590 71.0026 55.3481 0003473 142.6397 217.4968 14.17122540981849
| Epoch (UTC): | 15 July 2025 22:45:57 |
| Eccentricity: | 0.0003473 |
| inclination: | 71.0026° |
| perigee height: | 832 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 55.3481° |
| argument of perigee: | 142.6397° |
| revolutions per day: | 14.17122540 |
| mean anomaly at epoch: | 217.4968° |
| orbit number at epoch: | 98184 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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