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 22221.82604084 .00000634 00000-0 67865-4 0 9999
2 43678 97.9777 355.7394 0011153 106.3446 253.8973 14.92246097205814
Epoch (UTC): | 09 August 2022 19:49:29 |
Eccentricity: | 0.0011153 |
inclination: | 97.9777° |
perigee height: | 583 km |
apogee height: | 599 km |
right ascension of ascending node: | 355.7394° |
argument of perigee: | 106.3446° |
revolutions per day: | 14.92246097 |
mean anomaly at epoch: | 253.8973° |
orbit number at epoch: | 20581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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