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 55214U 22151WF 24358.04470016 .00014565 00000-0 27417-2 0 9996
2 55214 98.4848 18.7621 0124226 111.3365 250.1146 14.59788234106223
Epoch (UTC): | 23 December 2024 01:04:22 |
Eccentricity: | 0.0124226 |
inclination: | 98.4848° |
perigee height: | 606 km |
apogee height: | 782 km |
right ascension of ascending node: | 18.7621° |
argument of perigee: | 111.3365° |
revolutions per day: | 14.59788234 |
mean anomaly at epoch: | 250.1146° |
orbit number at epoch: | 10622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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