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 43678U 18084H 23080.27344926 .00002844 00000-0 27882-3 0 9997
2 43678 98.0046 222.5665 0010776 92.5290 267.7172 14.93040501239141
| Epoch (UTC): | 21 March 2023 06:33:46 |
| Eccentricity: | 0.0010776 |
| inclination: | 98.0046° |
| perigee height: | 581 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 222.5665° |
| argument of perigee: | 92.5290° |
| revolutions per day: | 14.93040501 |
| mean anomaly at epoch: | 267.7172° |
| orbit number at epoch: | 23914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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