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 32785U 08021C 23085.83799711 .00006342 00000-0 63758-3 0 9996
2 32785 97.6980 53.6412 0013132 25.4243 334.7619 14.91510156808616
| Epoch (UTC): | 26 March 2023 20:06:42 |
| Eccentricity: | 0.0013132 |
| inclination: | 97.6980° |
| perigee height: | 584 km |
| apogee height: | 602 km |
| right ascension of ascending node: | 53.6412° |
| argument of perigee: | 25.4243° |
| revolutions per day: | 14.91510156 |
| mean anomaly at epoch: | 334.7619° |
| orbit number at epoch: | 80861 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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