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 20441U 90005F 24259.94552144 .00000852 00000-0 32467-3 0 9991
2 20441 98.9001 259.5624 0010273 297.6593 119.4398 14.33544483810459
Epoch (UTC): | 15 September 2024 22:41:33 |
Eccentricity: | 0.0010273 |
inclination: | 98.9001° |
perigee height: | 772 km |
apogee height: | 787 km |
right ascension of ascending node: | 259.5624° |
argument of perigee: | 297.6593° |
revolutions per day: | 14.33544483 |
mean anomaly at epoch: | 119.4398° |
orbit number at epoch: | 81045 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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