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 40021U 14033M 24357.71734132 .00026424 00000-0 13062-2 0 9999
2 40021 98.1006 352.7583 0010397 165.6513 194.5016 15.17774921572614
Epoch (UTC): | 22 December 2024 17:12:58 |
Eccentricity: | 0.0010397 |
inclination: | 98.1006° |
perigee height: | 505 km |
apogee height: | 520 km |
right ascension of ascending node: | 352.7583° |
argument of perigee: | 165.6513° |
revolutions per day: | 15.17774921 |
mean anomaly at epoch: | 194.5016° |
orbit number at epoch: | 57261 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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