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 60649U 24140BA 24357.50274778 .00001920 00000-0 43156-3 0 9991
2 60649 88.9997 334.7321 0111952 316.4102 42.8299 14.52314665 19748
Epoch (UTC): | 22 December 2024 12:03:57 |
Eccentricity: | 0.0111952 |
inclination: | 88.9997° |
perigee height: | 638 km |
apogee height: | 797 km |
right ascension of ascending node: | 334.7321° |
argument of perigee: | 316.4102° |
revolutions per day: | 14.52314665 |
mean anomaly at epoch: | 42.8299° |
orbit number at epoch: | 1974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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