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 11574U 79089B 22227.40318629 .00000114 00000-0 43487-4 0 9995
2 11574 74.0718 338.6707 0014980 124.8544 235.4023 14.40917991248447
| Epoch (UTC): | 15 August 2022 09:40:35 |
| Eccentricity: | 0.0014980 |
| inclination: | 74.0718° |
| perigee height: | 745 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 338.6707° |
| argument of perigee: | 124.8544° |
| revolutions per day: | 14.40917991 |
| mean anomaly at epoch: | 235.4023° |
| orbit number at epoch: | 24844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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