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 22182.79972071 .00000727 00000-0 77127-4 0 9990
2 43678 97.9725 316.2342 0008673 232.7482 127.2961 14.92192200199997
| Epoch (UTC): | 01 July 2022 19:11:35 |
| Eccentricity: | 0.0008673 |
| inclination: | 97.9725° |
| perigee height: | 585 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 316.2342° |
| argument of perigee: | 232.7482° |
| revolutions per day: | 14.92192200 |
| mean anomaly at epoch: | 127.2961° |
| orbit number at epoch: | 19999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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