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 54881U 22151PS 24276.98790075 .00054551 00000-0 12336-1 0 9999
2 54881 98.4452 285.2249 0121003 25.5618 335.1493 14.51471706 97961
Epoch (UTC): | 02 October 2024 23:42:34 |
Eccentricity: | 0.0121003 |
inclination: | 98.4452° |
perigee height: | 635 km |
apogee height: | 807 km |
right ascension of ascending node: | 285.2249° |
argument of perigee: | 25.5618° |
revolutions per day: | 14.51471706 |
mean anomaly at epoch: | 335.1493° |
orbit number at epoch: | 9796 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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