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 22137.06601647 .00001233 00000-0 12697-3 0 9991
2 43678 97.9651 269.9735 0010637 36.6224 323.5743 14.92110295193170
Epoch (UTC): | 17 May 2022 01:35:03 |
Eccentricity: | 0.0010637 |
inclination: | 97.9651° |
perigee height: | 584 km |
apogee height: | 599 km |
right ascension of ascending node: | 269.9735° |
argument of perigee: | 36.6224° |
revolutions per day: | 14.92110295 |
mean anomaly at epoch: | 323.5743° |
orbit number at epoch: | 19317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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