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 11U 59001A 22332.34760132 .00000536 00000-0 26522-3 0 9999
2 11 32.8792 298.1458 1465465 259.4902 83.7812 11.86228854722863
| Epoch (UTC): | 28 November 2022 08:20:32 |
| Eccentricity: | 0.1465465 |
| inclination: | 32.8792° |
| perigee height: | 553 km |
| apogee height: | 2933 km |
| right ascension of ascending node: | 298.1458° |
| argument of perigee: | 259.4902° |
| revolutions per day: | 11.86228854 |
| mean anomaly at epoch: | 83.7812° |
| orbit number at epoch: | 72286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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