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 55224U 22151WR 24280.33162199 .00077201 00000-0 12468-1 0 9998
2 55224 98.6922 318.8523 0077466 356.8948 3.1765 14.68963941 95039
Epoch (UTC): | 06 October 2024 07:57:32 |
Eccentricity: | 0.0077466 |
inclination: | 98.6922° |
perigee height: | 610 km |
apogee height: | 719 km |
right ascension of ascending node: | 318.8523° |
argument of perigee: | 356.8948° |
revolutions per day: | 14.68963941 |
mean anomaly at epoch: | 3.1765° |
orbit number at epoch: | 9503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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