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 32225U 99025CVX 24280.86174593 .00001645 00000-0 89461-3 0 9995
2 32225 99.1496 315.6317 0071863 342.3888 17.4793 14.12447290620183
Epoch (UTC): | 06 October 2024 20:40:54 |
Eccentricity: | 0.0071863 |
inclination: | 99.1496° |
perigee height: | 799 km |
apogee height: | 903 km |
right ascension of ascending node: | 315.6317° |
argument of perigee: | 342.3888° |
revolutions per day: | 14.12447290 |
mean anomaly at epoch: | 17.4793° |
orbit number at epoch: | 62018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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