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 46294U 20061Y 24357.75095738 .00046573 00000-0 93512-3 0 9997
2 46294 97.3279 63.6328 0001629 200.5970 159.5214 15.46529374238436
Epoch (UTC): | 22 December 2024 18:01:22 |
Eccentricity: | 0.0001629 |
inclination: | 97.3279° |
perigee height: | 426 km |
apogee height: | 428 km |
right ascension of ascending node: | 63.6328° |
argument of perigee: | 200.5970° |
revolutions per day: | 15.46529374 |
mean anomaly at epoch: | 159.5214° |
orbit number at epoch: | 23843 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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